View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 41245U 00055EV 24280.35410533 .00008325 00000-0 42059-2 0 9996
2 41245 98.5825 313.6501 0017045 75.7146 284.5920 14.16332334450875
| Epoch (UTC): | 06 October 2024 08:29:54 |
| Eccentricity: | 0.0017045 |
| inclination: | 98.5825° |
| perigee height: | 825 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 313.6501° |
| argument of perigee: | 75.7146° |
| revolutions per day: | 14.16332334 |
| mean anomaly at epoch: | 284.5920° |
| orbit number at epoch: | 45087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|