View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 02520U 26151.63655272 +.00000000 +00000-0 -12450-2 0 00008
2 02520 89.8495 31.5650 0014456 328.1443 31.8533 8.58893886 05
| Epoch (UTC): | 31 May 2026 15:16:38 |
| Eccentricity: | 0.0014456 |
| inclination: | 89.8495° |
| perigee height: | 3679 km |
| apogee height: | 3708 km |
| right ascension of ascending node: | 31.5650° |
| argument of perigee: | 328.1443° |
| revolutions per day: | 8.58893886 |
| mean anomaly at epoch: | 31.8533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|