View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21938U 26068.32935205 +.00000000 +00000-0 +65397-4 0 00001
2 21938 82.9338 154.0291 0027696 299.8606 125.3473 13.75549437 03
| Epoch (UTC): | 09 March 2026 07:54:16 |
| Eccentricity: | 0.0027696 |
| inclination: | 82.9338° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 154.0291° |
| argument of perigee: | 299.8606° |
| revolutions per day: | 13.75549437 |
| mean anomaly at epoch: | 125.3473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|