View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13807U 26087.49683844 +.00000000 +00000-0 +15689-2 0 00002
2 13807 82.9442 90.9500 0009328 301.7931 58.2347 14.31473070 08
| Epoch (UTC): | 28 March 2026 11:55:26 |
| Eccentricity: | 0.0009328 |
| inclination: | 82.9442° |
| perigee height: | 780 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 90.9500° |
| argument of perigee: | 301.7931° |
| revolutions per day: | 14.31473070 |
| mean anomaly at epoch: | 58.2347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|