View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00022U 26129.89542098 +.00000000 +00000-0 +22021-3 0 00002
2 00022 50.2445 289.3541 0079378 329.7177 29.9209 15.28071586 02
| Epoch (UTC): | 09 May 2026 21:29:24 |
| Eccentricity: | 0.0079378 |
| inclination: | 50.2445° |
| perigee height: | 427 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 289.3541° |
| argument of perigee: | 329.7177° |
| revolutions per day: | 15.28071586 |
| mean anomaly at epoch: | 29.9209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|