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| -rw-r--r-- | README.md | 48 |
1 files changed, 24 insertions, 24 deletions
diff --git a/README.md b/README.md index 58871ab..06e3717 100644 --- a/README.md +++ b/README.md @@ -19,32 +19,32 @@ Implementing the "Two-line element set (TLE)", a data format encoding orbital el | Field | Columns | Content | Example | | ----- | ------- | ------- | ------- | -| 1 | 01-01 | Line number | 1 | -| 2 | 03–07 | Satellite number | 25544 | -| 3 | 08–08 | Classification (U=Unclassified) | U | -| 4 | 10–11 | International Designator (Last two digits of launch year) | 98 | -| 5 | 12–14 | International Designator (Launch number of the year) | 067 | -| 6 | 15–17 | International Designator (piece of the launch) | A | -| 7 | 19–20 | Epoch Year (last two digits of year) | 08 | -| 8 | 21–32 | Epoch (day of the year and fractional portion of the day) | 264.51782528 | -| 9 | 34–43 | First Time Derivative of the Mean Motion divided by two [11] | −.00002182 | -| 10 | 45–52 | Second Time Derivative of Mean Motion divided by six (decimal point assumed) | 00000-0 | -| 11 | 54–61 | BSTAR drag term (decimal point assumed) [11] | -11606-4 | -| 12 | 63–63 | The number 0 (originally this should have been "Ephemeris type") | 0 | -| 13 | 65–68 | Element set number. Incremented when a new TLE is generated for this object.[11] | 292 | -| 14 | 69–69 | Checksum (modulo 10) | 7 | +| 1 | 01-01 | Line number | `1` | +| 2 | 03–07 | Satellite number | `25544` | +| 3 | 08–08 | Classification (U=Unclassified) | `U` | +| 4 | 10–11 | International Designator (Last two digits of launch year) | `98` | +| 5 | 12–14 | International Designator (Launch number of the year) | `067` | +| 6 | 15–17 | International Designator (piece of the launch) | `A` | +| 7 | 19–20 | Epoch Year (last two digits of year) | `08` | +| 8 | 21–32 | Epoch (day of the year and fractional portion of the day) | `264.51782528` | +| 9 | 34–43 | First Time Derivative of the Mean Motion divided by two [11] | `−.00002182` | +| 10 | 45–52 | Second Time Derivative of Mean Motion divided by six (decimal point assumed) | `00000-0` | +| 11 | 54–61 | BSTAR drag term (decimal point assumed) [11] | `-11606-4` | +| 12 | 63–63 | The number 0 (originally this should have been "Ephemeris type") | `0` | +| 13 | 65–68 | Element set number. Incremented when a new TLE is generated for this object.[11] | `292` | +| 14 | 69–69 | Checksum (modulo 10) | `7`| ### Line two | Field | Columns | Content | Example | | ----- | ------- | ------- | ------- | -| 1 | 01–01 | Line number | 2 | -| 2 | 03–07 | Satellite number | 25544 | -| 3 | 09–16 | Inclination (degrees) | 51.6416 | -| 4 | 18–25 | Right ascension of the ascending node (degrees) | 247.4627 | -| 5 | 27–33 | Eccentricity (decimal point assumed) | 0006703 | -| 6 | 35–42 | Argument of perigee (degrees) | 130.5360 | -| 7 | 44–51 | Mean Anomaly (degrees) | 325.0288 | -| 8 | 53–63 | Mean Motion (revolutions per day) | 15.72125391 | -| 9 | 64–68 | Revolution number at epoch (revolutions) | 56353 | -| 10 | 69–69 | Checksum (modulo 10) | 7 | +| 1 | 01–01 | Line number | `2` | +| 2 | 03–07 | Satellite number | `25544` | +| 3 | 09–16 | Inclination (degrees) | `51.6416` | +| 4 | 18–25 | Right ascension of the ascending node (degrees) | `247.4627` | +| 5 | 27–33 | Eccentricity (decimal point assumed) | `0006703` | +| 6 | 35–42 | Argument of perigee (degrees) | `130.5360` | +| 7 | 44–51 | Mean Anomaly (degrees) | `325.0288` | +| 8 | 53–63 | Mean Motion (revolutions per day) | `15.72125391` | +| 9 | 64–68 | Revolution number at epoch (revolutions) | `56353` | +| 10 | 69–69 | Checksum (modulo 10) | `7` | |
