View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57533U 26145.60777248 +.00000000 +00000-0 +44874-4 0 00006
2 57533 43.0048 28.7706 0001432 280.1180 79.9510 15.27574453 08
| Epoch (UTC): | 25 May 2026 14:35:11 |
| Eccentricity: | 0.0001432 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 28.7706° |
| argument of perigee: | 280.1180° |
| revolutions per day: | 15.27574453 |
| mean anomaly at epoch: | 79.9510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|