View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23088U 26067.01830199 +.00000000 +00000-0 -87459-4 0 00004
2 23088 70.9986 74.3976 0005705 287.2652 72.7846 14.15012522 04
| Epoch (UTC): | 08 March 2026 00:26:21 |
| Eccentricity: | 0.0005705 |
| inclination: | 70.9986° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 74.3976° |
| argument of perigee: | 287.2652° |
| revolutions per day: | 14.15012522 |
| mean anomaly at epoch: | 72.7846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|