View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39679U 26042.19533837 +.00000000 +00000-0 +30621-3 0 00005
2 39679 51.6068 106.4386 0098914 6.4393 353.7836 15.38313107 03
| Epoch (UTC): | 11 February 2026 04:41:17 |
| Eccentricity: | 0.0098914 |
| inclination: | 51.6068° |
| perigee height: | 384 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 106.4386° |
| argument of perigee: | 6.4393° |
| revolutions per day: | 15.38313107 |
| mean anomaly at epoch: | 353.7836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|