View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00022U 26083.91061764 +.00000000 +00000-0 +37964-3 0 00002
2 00022 50.2432 156.3385 0080043 144.8504 215.7773 15.27116731 00
| Epoch (UTC): | 24 March 2026 21:51:17 |
| Eccentricity: | 0.0080043 |
| inclination: | 50.2432° |
| perigee height: | 430 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 156.3385° |
| argument of perigee: | 144.8504° |
| revolutions per day: | 15.27116731 |
| mean anomaly at epoch: | 215.7773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|