View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47907U 26145.41316477 +.00000000 +00000-0 +58360-4 0 00007
2 47907 53.1607 284.2730 0001604 93.1484 266.9701 15.31703727 04
| Epoch (UTC): | 25 May 2026 09:54:57 |
| Eccentricity: | 0.0001604 |
| inclination: | 53.1607° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 284.2730° |
| argument of perigee: | 93.1484° |
| revolutions per day: | 15.31703727 |
| mean anomaly at epoch: | 266.9701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|