View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66811U 26145.42186846 +.00000000 +00000-0 -56014-4 0 00003
2 66811 43.0044 41.0774 0000884 289.1767 70.8989 15.27556143 02
| Epoch (UTC): | 25 May 2026 10:07:29 |
| Eccentricity: | 0.0000884 |
| inclination: | 43.0044° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 41.0774° |
| argument of perigee: | 289.1767° |
| revolutions per day: | 15.27556143 |
| mean anomaly at epoch: | 70.8989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|