View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14085U 26022.20383172 +.00000000 +00000-0 +14478-3 0 00006
2 14085 82.9433 277.9607 0032784 323.9149 35.9795 13.76597536 02
| Epoch (UTC): | 22 January 2026 04:53:31 |
| Eccentricity: | 0.0032784 |
| inclination: | 82.9433° |
| perigee height: | 952 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 277.9607° |
| argument of perigee: | 323.9149° |
| revolutions per day: | 13.76597536 |
| mean anomaly at epoch: | 35.9795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|