View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25774U 99031E 24279.12682587 .00000387 00000-0 55666-3 0 9999
2 25774 51.5306 323.6532 0373565 283.3553 100.1762 13.46650751245768
| Epoch (UTC): | 05 October 2024 03:02:37 |
| Eccentricity: | 0.0373565 |
| inclination: | 51.5306° |
| perigee height: | 806 km |
| apogee height: | 1363 km |
| right ascension of ascending node: | 323.6532° |
| argument of perigee: | 283.3553° |
| revolutions per day: | 13.46650751 |
| mean anomaly at epoch: | 100.1762° |
| orbit number at epoch: | 24576 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|