View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21903U 26064.21042933 +.00000000 +00000-0 +70293-4 0 00005
2 21903 82.9415 345.5882 0041679 219.0170 307.4655 13.74743179 04
| Epoch (UTC): | 05 March 2026 05:03:01 |
| Eccentricity: | 0.0041679 |
| inclination: | 82.9415° |
| perigee height: | 952 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 345.5882° |
| argument of perigee: | 219.0170° |
| revolutions per day: | 13.74743179 |
| mean anomaly at epoch: | 307.4655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|