View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68046U 26145.33335647 +.00000000 +00000-0 -18507-3 0 00004
2 68046 53.1601 53.9570 0001024 82.9976 205.6621 15.34390693 04
| Epoch (UTC): | 25 May 2026 08:00:01 |
| Eccentricity: | 0.0001024 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 53.9570° |
| argument of perigee: | 82.9976° |
| revolutions per day: | 15.34390693 |
| mean anomaly at epoch: | 205.6621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|