View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57082U 26145.38429845 +.00000000 +00000-0 +14301-3 0 00008
2 57082 43.0052 22.6656 0001034 284.2494 75.8242 15.27565717 00
| Epoch (UTC): | 25 May 2026 09:13:23 |
| Eccentricity: | 0.0001034 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 22.6656° |
| argument of perigee: | 284.2494° |
| revolutions per day: | 15.27565717 |
| mean anomaly at epoch: | 75.8242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|