View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45416U 26060.58072375 +.00000000 +00000-0 +33563-3 0 00007
2 45416 53.0199 78.8814 0002168 268.4541 91.6260 16.45864176 04
| Epoch (UTC): | 01 March 2026 13:56:14 |
| Eccentricity: | 0.0002168 |
| inclination: | 53.0199° |
| perigee height: | 149 km |
| apogee height: | 152 km |
| right ascension of ascending node: | 78.8814° |
| argument of perigee: | 268.4541° |
| revolutions per day: | 16.45864176 |
| mean anomaly at epoch: | 91.6260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|