View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52480U 26145.53294287 +.00000000 +00000-0 -90832-4 0 00007
2 52480 53.2151 74.1552 0001511 89.3132 270.8033 15.08824875 07
| Epoch (UTC): | 25 May 2026 12:47:26 |
| Eccentricity: | 0.0001511 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.1552° |
| argument of perigee: | 89.3132° |
| revolutions per day: | 15.08824875 |
| mean anomaly at epoch: | 270.8033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|