View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65868U 26145.39793507 +.00000000 +00000-0 +69622-3 0 00005
2 65868 53.1612 297.6194 0001407 116.3366 243.7781 15.34408831 08
| Epoch (UTC): | 25 May 2026 09:33:01 |
| Eccentricity: | 0.0001407 |
| inclination: | 53.1612° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 297.6194° |
| argument of perigee: | 116.3366° |
| revolutions per day: | 15.34408831 |
| mean anomaly at epoch: | 243.7781° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|