View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53920U 26145.52699259 +.00000000 +00000-0 +24625-4 0 00000
2 53920 53.2147 329.2499 0001041 105.8832 254.2275 15.08837108 02
| Epoch (UTC): | 25 May 2026 12:38:52 |
| Eccentricity: | 0.0001041 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 329.2499° |
| argument of perigee: | 105.8832° |
| revolutions per day: | 15.08837108 |
| mean anomaly at epoch: | 254.2275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|