View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00876U 26069.93948816 +.00000000 +00000-0 +58404-4 0 00000
2 00876 65.0578 256.0407 0150093 297.5702 61.0220 14.65675721 03
| Epoch (UTC): | 10 March 2026 22:32:51 |
| Eccentricity: | 0.0150093 |
| inclination: | 65.0578° |
| perigee height: | 569 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 256.0407° |
| argument of perigee: | 297.5702° |
| revolutions per day: | 14.65675721 |
| mean anomaly at epoch: | 61.0220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|