View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10961U 26088.16013884 +.00000000 +00000-0 +92487-4 0 00009
2 10961 74.0749 235.2360 0015401 50.7213 309.5304 14.37579802 00
| Epoch (UTC): | 29 March 2026 03:50:35 |
| Eccentricity: | 0.0015401 |
| inclination: | 74.0749° |
| perigee height: | 756 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 235.2360° |
| argument of perigee: | 50.7213° |
| revolutions per day: | 14.37579802 |
| mean anomaly at epoch: | 309.5304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|