View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 10836U 76077CG 24357.88556818 -.00000040 00000-0 14897-4 0 9993
2 10836 102.0362 137.3240 0181645 267.3615 250.5660 12.07643028134318
| Epoch (UTC): | 22 December 2024 21:15:13 |
| Eccentricity: | 0.0181645 |
| inclination: | 102.0362° |
| perigee height: | 1501 km |
| apogee height: | 1792 km |
| right ascension of ascending node: | 137.3240° |
| argument of perigee: | 267.3615° |
| revolutions per day: | 12.07643028 |
| mean anomaly at epoch: | 250.5660° |
| orbit number at epoch: | 13431 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|