View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07714U 26075.18377279 +.00000000 +00000-0 +41783-4 0 00003
2 07714 81.1943 320.3403 0028465 252.6646 107.1409 14.08463981 04
| Epoch (UTC): | 16 March 2026 04:24:37 |
| Eccentricity: | 0.0028465 |
| inclination: | 81.1943° |
| perigee height: | 844 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 320.3403° |
| argument of perigee: | 252.6646° |
| revolutions per day: | 14.08463981 |
| mean anomaly at epoch: | 107.1409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|