View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 12457U 26088.17405168 +.00000000 +00000-0 +35461-4 0 00001
2 12457 81.2721 261.3052 0064695 118.6956 242.0738 14.07677216 04
| Epoch (UTC): | 29 March 2026 04:10:38 |
| Eccentricity: | 0.0064695 |
| inclination: | 81.2721° |
| perigee height: | 820 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 261.3052° |
| argument of perigee: | 118.6956° |
| revolutions per day: | 14.07677216 |
| mean anomaly at epoch: | 242.0738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|