View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 5024U 70025HY 23336.53303338 .00003524 00000-0 16144-2 0 9992
2 5024 99.8381 181.7119 0089096 202.7401 156.9814 14.20041047740409
| Epoch (UTC): | 02 December 2023 12:47:34 |
| Eccentricity: | 0.0089096 |
| inclination: | 99.8381° |
| perigee height: | 761 km |
| apogee height: | 889 km |
| right ascension of ascending node: | 181.7119° |
| argument of perigee: | 202.7401° |
| revolutions per day: | 14.20041047 |
| mean anomaly at epoch: | 156.9814° |
| orbit number at epoch: | 74040 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|