View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 11964U 26105.82816634 +.00000000 +00000-0 +00000-0 0 00006
2 11964 8.1204 303.4412 0032895 105.1463 242.0723 0.99234251 07
| Epoch (UTC): | 15 April 2026 19:52:33 |
| Eccentricity: | 0.0032895 |
| inclination: | 8.1204° |
| perigee height: | 35940 km |
| apogee height: | 36220 km |
| right ascension of ascending node: | 303.4412° |
| argument of perigee: | 105.1463° |
| revolutions per day: | 0.99234251 |
| mean anomaly at epoch: | 242.0723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|