View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10745U 26088.19391963 +.00000000 +00000-0 +18849-3 0 00008
2 10745 82.9222 116.7830 0036504 102.9700 325.8548 13.78914280 05
| Epoch (UTC): | 29 March 2026 04:39:14 |
| Eccentricity: | 0.0036504 |
| inclination: | 82.9222° |
| perigee height: | 941 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 116.7830° |
| argument of perigee: | 102.9700° |
| revolutions per day: | 13.78914280 |
| mean anomaly at epoch: | 325.8548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|