View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22590U 26053.77419442 +.00000000 +00000-0 +40090-4 0 00002
2 22590 82.9287 225.7097 0021840 251.8093 125.0450 13.75624952 02
| Epoch (UTC): | 22 February 2026 18:34:50 |
| Eccentricity: | 0.0021840 |
| inclination: | 82.9287° |
| perigee height: | 963 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 225.7097° |
| argument of perigee: | 251.8093° |
| revolutions per day: | 13.75624952 |
| mean anomaly at epoch: | 125.0450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|