View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 11267U 26038.19737819 +.00000000 +00000-0 +85043-4 0 00008
2 11267 82.5256 125.5027 0016691 154.7231 205.4809 14.91870419 07
| Epoch (UTC): | 07 February 2026 04:44:13 |
| Eccentricity: | 0.0016691 |
| inclination: | 82.5256° |
| perigee height: | 580 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 125.5027° |
| argument of perigee: | 154.7231° |
| revolutions per day: | 14.91870419 |
| mean anomaly at epoch: | 205.4809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|