View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14781U 26145.40003913 +.00000000 +00000-0 +11394-3 0 00003
2 14781 97.8044 111.2326 0006082 257.6923 102.3614 14.90719463 02
| Epoch (UTC): | 25 May 2026 09:36:03 |
| Eccentricity: | 0.0006082 |
| inclination: | 97.8044° |
| perigee height: | 591 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 111.2326° |
| argument of perigee: | 257.6923° |
| revolutions per day: | 14.90719463 |
| mean anomaly at epoch: | 102.3614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|