View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13000U 26065.58989536 +.00000000 +00000-0 -11141-2 0 00000
2 13000 82.9588 116.3733 0018129 27.5703 128.0742 12.06921096 05
| Epoch (UTC): | 06 March 2026 14:09:26 |
| Eccentricity: | 0.0018129 |
| inclination: | 82.9588° |
| perigee height: | 1635 km |
| apogee height: | 1665 km |
| right ascension of ascending node: | 116.3733° |
| argument of perigee: | 27.5703° |
| revolutions per day: | 12.06921096 |
| mean anomaly at epoch: | 128.0742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|