View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51863U 26144.94872831 +.00000000 +00000-0 +51399-5 0 00007
2 51863 53.2155 26.7800 0001322 93.2184 266.8959 15.08833523 07
| Epoch (UTC): | 24 May 2026 22:46:10 |
| Eccentricity: | 0.0001322 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 26.7800° |
| argument of perigee: | 93.2184° |
| revolutions per day: | 15.08833523 |
| mean anomaly at epoch: | 266.8959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|