View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51809U 26145.00668252 +.00000000 +00000-0 +10615-4 0 00000
2 51809 53.2163 356.4809 0001552 92.2861 267.8309 15.08837500 03
| Epoch (UTC): | 25 May 2026 00:09:37 |
| Eccentricity: | 0.0001552 |
| inclination: | 53.2163° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 356.4809° |
| argument of perigee: | 92.2861° |
| revolutions per day: | 15.08837500 |
| mean anomaly at epoch: | 267.8309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|