View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45088U 26145.57287454 +.00000000 +00000-0 +11299-2 0 00002
2 45088 53.1562 244.8640 0003234 335.5060 24.5788 15.33672034 09
| Epoch (UTC): | 25 May 2026 13:44:56 |
| Eccentricity: | 0.0003234 |
| inclination: | 53.1562° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 244.8640° |
| argument of perigee: | 335.5060° |
| revolutions per day: | 15.33672034 |
| mean anomaly at epoch: | 24.5788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|