View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62054U 26145.57213942 +.00000000 +00000-0 +52956-3 0 00001
2 62054 43.0005 182.1437 0001843 271.8218 88.2422 15.27595860 06
| Epoch (UTC): | 25 May 2026 13:43:52 |
| Eccentricity: | 0.0001843 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.1437° |
| argument of perigee: | 271.8218° |
| revolutions per day: | 15.27595860 |
| mean anomaly at epoch: | 88.2422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|