View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14781U 26071.82885625 +.00000000 +00000-0 +18702-3 0 00005
2 14781 97.7946 38.5566 0008619 134.6539 225.5383 14.90518657 07
| Epoch (UTC): | 12 March 2026 19:53:33 |
| Eccentricity: | 0.0008619 |
| inclination: | 97.7946° |
| perigee height: | 590 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 38.5566° |
| argument of perigee: | 134.6539° |
| revolutions per day: | 14.90518657 |
| mean anomaly at epoch: | 225.5383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|