View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24971U 97057A 24277.16438445 .00001593 00000-0 56778-3 0 9992
2 24971 98.7766 247.2857 0051367 259.6710 99.8681 14.34945855413383
| Epoch (UTC): | 03 October 2024 03:56:42 |
| Eccentricity: | 0.0051367 |
| inclination: | 98.7766° |
| perigee height: | 738 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 247.2857° |
| argument of perigee: | 259.6710° |
| revolutions per day: | 14.34945855 |
| mean anomaly at epoch: | 99.8681° |
| orbit number at epoch: | 41338 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|