View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27646U 26075.57160500 +.00000000 +00000-0 +74707-4 0 00001
2 27646 49.5194 263.6551 5410245 128.6666 320.6303 4.61718313 04
| Epoch (UTC): | 16 March 2026 13:43:06 |
| Eccentricity: | 0.5410245 |
| inclination: | 49.5194° |
| perigee height: | 614 km |
| apogee height: | 17098 km |
| right ascension of ascending node: | 263.6551° |
| argument of perigee: | 128.6666° |
| revolutions per day: | 4.61718313 |
| mean anomaly at epoch: | 320.6303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|