View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60391U 26145.54567412 +.00000000 +00000-0 +10829-3 0 00007
2 60391 88.9709 282.4065 0015025 96.6453 263.6409 13.51008339 08
| Epoch (UTC): | 25 May 2026 13:05:46 |
| Eccentricity: | 0.0015025 |
| inclination: | 88.9709° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 282.4065° |
| argument of perigee: | 96.6453° |
| revolutions per day: | 13.51008339 |
| mean anomaly at epoch: | 263.6409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|