View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20692U 26146.04359779 +.00000000 +00000-0 +42529-3 0 00000
2 20692 63.2944 269.5737 0874226 84.2830 285.7103 13.64495871 06
| Epoch (UTC): | 26 May 2026 01:02:46 |
| Eccentricity: | 0.0874226 |
| inclination: | 63.2944° |
| perigee height: | 373 km |
| apogee height: | 1666 km |
| right ascension of ascending node: | 269.5737° |
| argument of perigee: | 84.2830° |
| revolutions per day: | 13.64495871 |
| mean anomaly at epoch: | 285.7103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|