View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51813U 26145.58905171 +.00000000 +00000-0 +47421-4 0 00007
2 51813 53.2124 343.9349 0001282 91.8602 268.2537 15.08838562 00
| Epoch (UTC): | 25 May 2026 14:08:14 |
| Eccentricity: | 0.0001282 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 343.9349° |
| argument of perigee: | 91.8602° |
| revolutions per day: | 15.08838562 |
| mean anomaly at epoch: | 268.2537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|