View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 08788U 26073.00926507 +.00000000 +00000-0 +74955-4 0 00005
2 08788 102.0848 173.2531 0071046 260.6728 276.1666 12.39832982 08
| Epoch (UTC): | 14 March 2026 00:13:20 |
| Eccentricity: | 0.0071046 |
| inclination: | 102.0848° |
| perigee height: | 1451 km |
| apogee height: | 1563 km |
| right ascension of ascending node: | 173.2531° |
| argument of perigee: | 260.6728° |
| revolutions per day: | 12.39832982 |
| mean anomaly at epoch: | 276.1666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|