View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22287U 26069.84499839 +.00000000 +00000-0 +65788-4 0 00009
2 22287 82.5275 351.7894 0023217 336.1911 23.8226 14.80052871 07
| Epoch (UTC): | 10 March 2026 20:16:47 |
| Eccentricity: | 0.0023217 |
| inclination: | 82.5275° |
| perigee height: | 613 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 351.7894° |
| argument of perigee: | 336.1911° |
| revolutions per day: | 14.80052871 |
| mean anomaly at epoch: | 23.8226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|