View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52863U 26145.43862856 +.00000000 +00000-0 +11970-4 0 00009
2 52863 53.2126 39.5811 0001109 94.4648 265.6470 15.08838645 06
| Epoch (UTC): | 25 May 2026 10:31:37 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.5811° |
| argument of perigee: | 94.4648° |
| revolutions per day: | 15.08838645 |
| mean anomaly at epoch: | 265.6470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|