View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62767U 26145.58335647 +.00000000 +00000-0 -23308-4 0 00001
2 62767 53.1603 325.1670 0001189 92.9310 341.0527 15.34394728 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 325.1670° |
| argument of perigee: | 92.9310° |
| revolutions per day: | 15.34394728 |
| mean anomaly at epoch: | 341.0527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|