View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23774U 26159.29846207 +.00000000 +00000-0 +28201-4 0 00004
2 23774 82.9786 98.7811 0043795 169.8292 190.3763 13.76852803 06
| Epoch (UTC): | 08 June 2026 07:09:47 |
| Eccentricity: | 0.0043795 |
| inclination: | 82.9786° |
| perigee height: | 943 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 98.7811° |
| argument of perigee: | 169.8292° |
| revolutions per day: | 13.76852803 |
| mean anomaly at epoch: | 190.3763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|