View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27386U 26161.51548074 +.00000000 +00000-0 +35667-4 0 00000
2 27386 98.3831 112.9828 0001340 90.0685 26.5865 14.39063279 03
| Epoch (UTC): | 10 June 2026 12:22:17 |
| Eccentricity: | 0.0001340 |
| inclination: | 98.3831° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 112.9828° |
| argument of perigee: | 90.0685° |
| revolutions per day: | 14.39063279 |
| mean anomaly at epoch: | 26.5865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|