View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21153U 26071.79657531 +.00000000 +00000-0 +53459-4 0 00004
2 21153 82.9299 348.7579 0027803 235.0314 177.9558 13.76344500 09
| Epoch (UTC): | 12 March 2026 19:07:04 |
| Eccentricity: | 0.0027803 |
| inclination: | 82.9299° |
| perigee height: | 956 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 348.7579° |
| argument of perigee: | 235.0314° |
| revolutions per day: | 13.76344500 |
| mean anomaly at epoch: | 177.9558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|