View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21796U 26053.86134192 +.00000000 +00000-0 +44265-4 0 00003
2 21796 82.9513 255.4173 0048118 302.1174 72.9577 13.75752625 02
| Epoch (UTC): | 22 February 2026 20:40:19 |
| Eccentricity: | 0.0048118 |
| inclination: | 82.9513° |
| perigee height: | 944 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 255.4173° |
| argument of perigee: | 302.1174° |
| revolutions per day: | 13.75752625 |
| mean anomaly at epoch: | 72.9577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|