View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68965U 26145.58335647 +.00000000 +00000-0 -19799-1 0 00003
2 68965 53.1596 267.8893 0001310 68.6880 123.5692 15.67345126 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001310 |
| inclination: | 53.1596° |
| perigee height: | 366 km |
| apogee height: | 367 km |
| right ascension of ascending node: | 267.8893° |
| argument of perigee: | 68.6880° |
| revolutions per day: | 15.67345126 |
| mean anomaly at epoch: | 123.5692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|