View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25515U 26065.45763625 +.00000000 +00000-0 +00000-0 0 00008
2 25515 10.0030 50.7056 0003078 251.2111 121.4828 0.99005496 06
| Epoch (UTC): | 06 March 2026 10:58:59 |
| Eccentricity: | 0.0003078 |
| inclination: | 10.0030° |
| perigee height: | 36132 km |
| apogee height: | 36158 km |
| right ascension of ascending node: | 50.7056° |
| argument of perigee: | 251.2111° |
| revolutions per day: | 0.99005496 |
| mean anomaly at epoch: | 121.4828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|