View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66961U 26145.46516422 +.00000000 +00000-0 +99008-3 0 00008
2 66961 42.9996 309.4895 0000639 279.1758 80.9021 15.27592144 04
| Epoch (UTC): | 25 May 2026 11:09:50 |
| Eccentricity: | 0.0000639 |
| inclination: | 42.9996° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 309.4895° |
| argument of perigee: | 279.1758° |
| revolutions per day: | 15.27592144 |
| mean anomaly at epoch: | 80.9021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|