View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44679U 26018.17663544 +.00000000 +00000-0 +00000-0 0 00006
2 44679 13.2710 51.5214 4692665 279.6558 31.9776 1.79402674 07
| Epoch (UTC): | 18 January 2026 04:14:21 |
| Eccentricity: | 0.4692665 |
| inclination: | 13.2710° |
| perigee height: | 8806 km |
| apogee height: | 35657 km |
| right ascension of ascending node: | 51.5214° |
| argument of perigee: | 279.6558° |
| revolutions per day: | 1.79402674 |
| mean anomaly at epoch: | 31.9776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|