View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00005U 26134.89553611 +.00000000 +00000-0 +13755-3 0 00006
2 00005 34.2482 57.0677 1836008 348.3595 7.9502 10.85981134 08
| Epoch (UTC): | 14 May 2026 21:29:34 |
| Eccentricity: | 0.1836008 |
| inclination: | 34.2482° |
| perigee height: | 654 km |
| apogee height: | 3817 km |
| right ascension of ascending node: | 57.0677° |
| argument of perigee: | 348.3595° |
| revolutions per day: | 10.85981134 |
| mean anomaly at epoch: | 7.9502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|