View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40968U 26156.44553154 +.00000000 +00000-0 +35342-3 0 00001
2 40968 64.7763 295.6808 0118390 57.7878 303.4649 14.95824911 07
| Epoch (UTC): | 05 June 2026 10:41:33 |
| Eccentricity: | 0.0118390 |
| inclination: | 64.7763° |
| perigee height: | 497 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 295.6808° |
| argument of perigee: | 57.7878° |
| revolutions per day: | 14.95824911 |
| mean anomaly at epoch: | 303.4649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|