View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00836U 26155.01697654 +.00000000 +00000-0 +00000-0 0 00007
2 00836 52.8642 118.8186 5106413 276.5091 0.6221 0.23915798 04
| Epoch (UTC): | 04 June 2026 00:24:26 |
| Eccentricity: | 0.5106413 |
| inclination: | 52.8642° |
| perigee height: | 47272 km |
| apogee height: | 159240 km |
| right ascension of ascending node: | 118.8186° |
| argument of perigee: | 276.5091° |
| revolutions per day: | 0.23915798 |
| mean anomaly at epoch: | 0.6221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|