View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27646U 26040.08796412 +.00000000 +00000-0 +31443-3 0 00005
2 27646 49.5153 285.5000 5414812 110.0060 20.5610 4.61714571 07
| Epoch (UTC): | 09 February 2026 02:06:40 |
| Eccentricity: | 0.5414812 |
| inclination: | 49.5153° |
| perigee height: | 607 km |
| apogee height: | 17105 km |
| right ascension of ascending node: | 285.5000° |
| argument of perigee: | 110.0060° |
| revolutions per day: | 4.61714571 |
| mean anomaly at epoch: | 20.5610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|