View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07615U 26088.15791558 +.00000000 +00000-0 +23994-3 0 00007
2 07615 99.0317 44.7008 0008798 163.3400 196.8053 13.96967022 09
| Epoch (UTC): | 29 March 2026 03:47:23 |
| Eccentricity: | 0.0008798 |
| inclination: | 99.0317° |
| perigee height: | 898 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 44.7008° |
| argument of perigee: | 163.3400° |
| revolutions per day: | 13.96967022 |
| mean anomaly at epoch: | 196.8053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|