View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 09510U 26068.38774712 +.00000000 +00000-0 +86042-4 0 00003
2 09510 82.9411 171.7191 0024833 252.7863 107.0576 13.77881433 03
| Epoch (UTC): | 09 March 2026 09:18:21 |
| Eccentricity: | 0.0024833 |
| inclination: | 82.9411° |
| perigee height: | 953 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 171.7191° |
| argument of perigee: | 252.7863° |
| revolutions per day: | 13.77881433 |
| mean anomaly at epoch: | 107.0576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|