View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68055U 26145.58335647 +.00000000 +00000-0 +20325-2 0 00000
2 68055 53.1604 52.8526 0001051 106.0643 89.3673 15.34382099 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001051 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 52.8526° |
| argument of perigee: | 106.0643° |
| revolutions per day: | 15.34382099 |
| mean anomaly at epoch: | 89.3673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|