View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48286U 26145.52121534 +.00000000 +00000-0 -60258-4 0 00008
2 48286 53.1592 78.1021 0001243 93.0834 267.0309 15.31703073 08
| Epoch (UTC): | 25 May 2026 12:30:33 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 78.1021° |
| argument of perigee: | 93.0834° |
| revolutions per day: | 15.31703073 |
| mean anomaly at epoch: | 267.0309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|