View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56165U 26088.20572512 +.00000000 +00000-0 +77634-4 0 00005
2 56165 81.0050 148.6598 0007599 157.5913 202.5576 13.85237039 09
| Epoch (UTC): | 29 March 2026 04:56:14 |
| Eccentricity: | 0.0007599 |
| inclination: | 81.0050° |
| perigee height: | 940 km |
| apogee height: | 951 km |
| right ascension of ascending node: | 148.6598° |
| argument of perigee: | 157.5913° |
| revolutions per day: | 13.85237039 |
| mean anomaly at epoch: | 202.5576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|