View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 36108U 09068A 23081.39979897 -.00000073 00000-0 00000+0 0 9996
2 36108 0.2995 92.8739 0000215 137.6810 104.8150 0.99452023 48642
| Epoch (UTC): | 22 March 2023 09:35:42 |
| Eccentricity: | 0.0000215 |
| inclination: | 0.2995° |
| perigee height: | 36016 km |
| apogee height: | 36018 km |
| right ascension of ascending node: | 92.8739° |
| argument of perigee: | 137.6810° |
| revolutions per day: | 0.99452023 |
| mean anomaly at epoch: | 104.8150° |
| orbit number at epoch: | 4864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|