View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51120U 26145.42808610 +.00000000 +00000-0 +78836-4 0 00005
2 51120 53.2128 304.6390 0001281 87.2671 272.8468 15.08840808 09
| Epoch (UTC): | 25 May 2026 10:16:26 |
| Eccentricity: | 0.0001281 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.6390° |
| argument of perigee: | 87.2671° |
| revolutions per day: | 15.08840808 |
| mean anomaly at epoch: | 272.8468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|