View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32953U 08025A 25317.17495557 .00000067 00000-0 41069-3 0 9994
2 32953 82.4992 129.8128 0019856 64.3236 295.9891 12.43170637792850
| Epoch (UTC): | 13 November 2025 04:11:56 |
| Eccentricity: | 0.0019856 |
| inclination: | 82.4992° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 129.8128° |
| argument of perigee: | 64.3236° |
| revolutions per day: | 12.43170637 |
| mean anomaly at epoch: | 295.9891° |
| orbit number at epoch: | 79285 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|