View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39679U 26069.14835709 +.00000000 +00000-0 +40816-3 0 00009
2 39679 51.6079 335.0419 0097453 104.7108 256.4701 15.39198695 09
| Epoch (UTC): | 10 March 2026 03:33:38 |
| Eccentricity: | 0.0097453 |
| inclination: | 51.6079° |
| perigee height: | 382 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 335.0419° |
| argument of perigee: | 104.7108° |
| revolutions per day: | 15.39198695 |
| mean anomaly at epoch: | 256.4701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|