View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21903U 26076.20838697 +.00000000 +00000-0 +63006-4 0 00001
2 21903 82.9405 336.7010 0042406 185.0385 286.8173 13.74744608 00
| Epoch (UTC): | 17 March 2026 05:00:04 |
| Eccentricity: | 0.0042406 |
| inclination: | 82.9405° |
| perigee height: | 951 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 336.7010° |
| argument of perigee: | 185.0385° |
| revolutions per day: | 13.74744608 |
| mean anomaly at epoch: | 286.8173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|