View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52331U 26145.48600465 +.00000000 +00000-0 +40382-4 0 00009
2 52331 53.2136 224.3699 0000963 81.3207 278.7894 15.08840959 04
| Epoch (UTC): | 25 May 2026 11:39:50 |
| Eccentricity: | 0.0000963 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 224.3699° |
| argument of perigee: | 81.3207° |
| revolutions per day: | 15.08840959 |
| mean anomaly at epoch: | 278.7894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|