View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48054U 26145.19884767 +.00000000 +00000-0 -96241-4 0 00009
2 48054 87.8949 324.7959 0001783 80.7009 279.4322 13.13467387 02
| Epoch (UTC): | 25 May 2026 04:46:20 |
| Eccentricity: | 0.0001783 |
| inclination: | 87.8949° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7959° |
| argument of perigee: | 80.7009° |
| revolutions per day: | 13.13467387 |
| mean anomaly at epoch: | 279.4322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|