View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53851U 26145.18927712 +.00000000 +00000-0 +60113-4 0 00005
2 53851 53.2137 310.4746 0001190 88.1272 271.9857 15.08843558 05
| Epoch (UTC): | 25 May 2026 04:32:33 |
| Eccentricity: | 0.0001190 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 310.4746° |
| argument of perigee: | 88.1272° |
| revolutions per day: | 15.08843558 |
| mean anomaly at epoch: | 271.9857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|