View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25134U 26134.82516970 +.00000000 +00000-0 +00000-0 0 00002
2 25134 12.7905 10.9835 0003083 170.0291 26.2058 0.99152015 06
| Epoch (UTC): | 14 May 2026 19:48:14 |
| Eccentricity: | 0.0003083 |
| inclination: | 12.7905° |
| perigee height: | 36090 km |
| apogee height: | 36117 km |
| right ascension of ascending node: | 10.9835° |
| argument of perigee: | 170.0291° |
| revolutions per day: | 0.99152015 |
| mean anomaly at epoch: | 26.2058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|