View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 09444U 26160.02785948 +.00000000 +00000-0 +55814-4 0 00009
2 09444 74.0515 21.4870 0012066 69.8807 290.3645 14.39379817 01
| Epoch (UTC): | 09 June 2026 00:40:07 |
| Eccentricity: | 0.0012066 |
| inclination: | 74.0515° |
| perigee height: | 752 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 21.4870° |
| argument of perigee: | 69.8807° |
| revolutions per day: | 14.39379817 |
| mean anomaly at epoch: | 290.3645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|