View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 09662U 26160.08763522 +.00000000 +00000-0 +73869-4 0 00001
2 09662 81.2738 180.4240 0050859 282.5429 77.0051 14.01307994 00
| Epoch (UTC): | 09 June 2026 02:06:11 |
| Eccentricity: | 0.0050859 |
| inclination: | 81.2738° |
| perigee height: | 852 km |
| apogee height: | 926 km |
| right ascension of ascending node: | 180.4240° |
| argument of perigee: | 282.5429° |
| revolutions per day: | 14.01307994 |
| mean anomaly at epoch: | 77.0051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|