View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54830U 26145.15505485 +.00000000 +00000-0 +40849-5 0 00004
2 54830 43.0047 64.5712 0001023 272.4386 87.6349 15.27573498 01
| Epoch (UTC): | 25 May 2026 03:43:16 |
| Eccentricity: | 0.0001023 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.5712° |
| argument of perigee: | 272.4386° |
| revolutions per day: | 15.27573498 |
| mean anomaly at epoch: | 87.6349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|