View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62642U 26145.48989852 +.00000000 +00000-0 +38344-3 0 00009
2 62642 97.4023 227.5698 0003259 47.4440 312.7074 15.28910520 05
| Epoch (UTC): | 25 May 2026 11:45:27 |
| Eccentricity: | 0.0003259 |
| inclination: | 97.4023° |
| perigee height: | 477 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 227.5698° |
| argument of perigee: | 47.4440° |
| revolutions per day: | 15.28910520 |
| mean anomaly at epoch: | 312.7074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|