View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53415U 26145.33099159 +.00000000 +00000-0 +10208-3 0 00002
2 53415 53.2150 130.0621 0001254 54.4478 305.6631 15.08852129 08
| Epoch (UTC): | 25 May 2026 07:56:37 |
| Eccentricity: | 0.0001254 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 130.0621° |
| argument of perigee: | 54.4478° |
| revolutions per day: | 15.08852129 |
| mean anomaly at epoch: | 305.6631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|