View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62285U 26145.46045042 +.00000000 +00000-0 +54053-3 0 00009
2 62285 43.0009 142.7455 0001996 292.4111 67.6530 15.27597705 09
| Epoch (UTC): | 25 May 2026 11:03:02 |
| Eccentricity: | 0.0001996 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 142.7455° |
| argument of perigee: | 292.4111° |
| revolutions per day: | 15.27597705 |
| mean anomaly at epoch: | 67.6530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|