View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00020U 26047.07053997 +.00000000 +00000-0 +40466-3 0 00007
2 00020 33.3446 342.9978 1638181 124.2663 252.4072 11.61826614 09
| Epoch (UTC): | 16 February 2026 01:41:34 |
| Eccentricity: | 0.1638181 |
| inclination: | 33.3446° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 342.9978° |
| argument of perigee: | 124.2663° |
| revolutions per day: | 11.61826614 |
| mean anomaly at epoch: | 252.4072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|