View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52831U 26145.15066245 +.00000000 +00000-0 -76662-4 0 00001
2 52831 53.2149 50.8702 0001406 89.8031 270.3123 15.08850091 02
| Epoch (UTC): | 25 May 2026 03:36:57 |
| Eccentricity: | 0.0001406 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 50.8702° |
| argument of perigee: | 89.8031° |
| revolutions per day: | 15.08850091 |
| mean anomaly at epoch: | 270.3123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|