View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45772U 26145.49502627 +.00000000 +00000-0 +92135-3 0 00004
2 45772 53.0435 176.0300 0003881 354.0703 6.0251 15.34091366 08
| Epoch (UTC): | 25 May 2026 11:52:50 |
| Eccentricity: | 0.0003881 |
| inclination: | 53.0435° |
| perigee height: | 461 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 176.0300° |
| argument of perigee: | 354.0703° |
| revolutions per day: | 15.34091366 |
| mean anomaly at epoch: | 6.0251° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|