View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64608U 26145.55277912 +.00000000 +00000-0 +62237-3 0 00006
2 64608 53.1589 338.1627 0001022 109.1442 250.9670 15.30217401 06
| Epoch (UTC): | 25 May 2026 13:16:00 |
| Eccentricity: | 0.0001022 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.1627° |
| argument of perigee: | 109.1442° |
| revolutions per day: | 15.30217401 |
| mean anomaly at epoch: | 250.9670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|