View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07275U 26088.12560310 +.00000000 +00000-0 +50922-4 0 00008
2 07275 81.2399 90.4092 0056236 209.0482 150.7556 14.07084298 08
| Epoch (UTC): | 29 March 2026 03:00:52 |
| Eccentricity: | 0.0056236 |
| inclination: | 81.2399° |
| perigee height: | 829 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 90.4092° |
| argument of perigee: | 209.0482° |
| revolutions per day: | 14.07084298 |
| mean anomaly at epoch: | 150.7556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|