View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62955U 26145.24281292 +.00000000 +00000-0 +59738-3 0 00003
2 62955 53.1607 236.4894 0001481 89.7772 270.3400 15.31718596 03
| Epoch (UTC): | 25 May 2026 05:49:39 |
| Eccentricity: | 0.0001481 |
| inclination: | 53.1607° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 236.4894° |
| argument of perigee: | 89.7772° |
| revolutions per day: | 15.31718596 |
| mean anomaly at epoch: | 270.3400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|