View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00022U 26134.79994696 +.00000000 +00000-0 +16645-3 0 00007
2 00022 50.2427 265.1280 0079283 349.5931 10.3385 15.28120810 01
| Epoch (UTC): | 14 May 2026 19:11:55 |
| Eccentricity: | 0.0079283 |
| inclination: | 50.2427° |
| perigee height: | 427 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 265.1280° |
| argument of perigee: | 349.5931° |
| revolutions per day: | 15.28120810 |
| mean anomaly at epoch: | 10.3385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|