View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39679U 26070.12223427 +.00000000 +00000-0 +41035-3 0 00001
2 39679 51.6080 330.2898 0097358 108.2387 252.9222 15.39237531 03
| Epoch (UTC): | 11 March 2026 02:56:01 |
| Eccentricity: | 0.0097358 |
| inclination: | 51.6080° |
| perigee height: | 382 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 330.2898° |
| argument of perigee: | 108.2387° |
| revolutions per day: | 15.39237531 |
| mean anomaly at epoch: | 252.9222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|