View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14085U 26074.89970699 +.00000000 +00000-0 -50609-4 0 00002
2 14085 82.9407 238.8084 0033676 172.4889 187.6780 13.76592665 04
| Epoch (UTC): | 15 March 2026 21:35:34 |
| Eccentricity: | 0.0033676 |
| inclination: | 82.9407° |
| perigee height: | 951 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 238.8084° |
| argument of perigee: | 172.4889° |
| revolutions per day: | 13.76592665 |
| mean anomaly at epoch: | 187.6780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|