View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48437U 26145.51686013 +.00000000 +00000-0 +25417-4 0 00000
2 48437 53.1587 193.7172 0001260 87.6750 272.4396 15.31696804 05
| Epoch (UTC): | 25 May 2026 12:24:16 |
| Eccentricity: | 0.0001260 |
| inclination: | 53.1587° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 193.7172° |
| argument of perigee: | 87.6750° |
| revolutions per day: | 15.31696804 |
| mean anomaly at epoch: | 272.4396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|