View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10967U 26076.10504270 +.00000000 +00000-0 +98556-4 0 00003
2 10967 108.0094 141.0597 0002425 282.7214 77.3660 14.46166392 04
| Epoch (UTC): | 17 March 2026 02:31:15 |
| Eccentricity: | 0.0002425 |
| inclination: | 108.0094° |
| perigee height: | 736 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 141.0597° |
| argument of perigee: | 282.7214° |
| revolutions per day: | 14.46166392 |
| mean anomaly at epoch: | 77.3660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|