View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38011U 26150.54706708 +.00000000 +00000-0 +25608-3 0 00001
2 38011 97.8079 211.3671 0001508 97.6213 39.9071 14.82464926 03
| Epoch (UTC): | 30 May 2026 13:07:46 |
| Eccentricity: | 0.0001508 |
| inclination: | 97.8079° |
| perigee height: | 620 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 211.3671° |
| argument of perigee: | 97.6213° |
| revolutions per day: | 14.82464926 |
| mean anomaly at epoch: | 39.9071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|