View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53706U 26144.60511384 +.00000000 +00000-0 -13942-5 0 00004
2 53706 53.2162 263.3845 0001330 89.3800 270.7345 15.08838825 04
| Epoch (UTC): | 24 May 2026 14:31:21 |
| Eccentricity: | 0.0001330 |
| inclination: | 53.2162° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 263.3845° |
| argument of perigee: | 89.3800° |
| revolutions per day: | 15.08838825 |
| mean anomaly at epoch: | 270.7345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|