View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 69035U 26145.58335647 +.00000000 +00000-0 -21393-1 0 00005
2 69035 97.2844 0.3472 0001960 100.8123 182.5824 15.64780562 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001960 |
| inclination: | 97.2844° |
| perigee height: | 373 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 0.3472° |
| argument of perigee: | 100.8123° |
| revolutions per day: | 15.64780562 |
| mean anomaly at epoch: | 182.5824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|