View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46572U 26145.58335647 +.00000000 +00000-0 +56084-3 0 00002
2 46572 53.0469 118.1221 0007627 96.2612 266.0296 15.82111153 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0007627 |
| inclination: | 53.0469° |
| perigee height: | 319 km |
| apogee height: | 330 km |
| right ascension of ascending node: | 118.1221° |
| argument of perigee: | 96.2612° |
| revolutions per day: | 15.82111153 |
| mean anomaly at epoch: | 266.0296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|