View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 06126U 26121.79313684 +.00000000 +00000-0 +24933-3 0 00005
2 06126 99.3402 150.7497 0008540 29.0886 331.0751 13.97833250 08
| Epoch (UTC): | 01 May 2026 19:02:07 |
| Eccentricity: | 0.0008540 |
| inclination: | 99.3402° |
| perigee height: | 895 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 150.7497° |
| argument of perigee: | 29.0886° |
| revolutions per day: | 13.97833250 |
| mean anomaly at epoch: | 331.0751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|