View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55053U 26145.56937796 +.00000000 +00000-0 +15038-3 0 00001
2 55053 97.3250 206.3732 0009263 187.1746 172.9366 15.33313164 07
| Epoch (UTC): | 25 May 2026 13:39:54 |
| Eccentricity: | 0.0009263 |
| inclination: | 97.3250° |
| perigee height: | 460 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 206.3732° |
| argument of perigee: | 187.1746° |
| revolutions per day: | 15.33313164 |
| mean anomaly at epoch: | 172.9366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|