View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53602U 26145.57891946 +.00000000 +00000-0 +37278-4 0 00007
2 53602 53.2151 253.8892 0001347 92.0762 268.0384 15.08839200 00
| Epoch (UTC): | 25 May 2026 13:53:38 |
| Eccentricity: | 0.0001347 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 253.8892° |
| argument of perigee: | 92.0762° |
| revolutions per day: | 15.08839200 |
| mean anomaly at epoch: | 268.0384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|