View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64666U 26145.39303304 +.00000000 +00000-0 +79415-3 0 00003
2 64666 53.1588 129.6383 0001401 35.3498 324.7598 15.34404993 00
| Epoch (UTC): | 25 May 2026 09:25:58 |
| Eccentricity: | 0.0001401 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 129.6383° |
| argument of perigee: | 35.3498° |
| revolutions per day: | 15.34404993 |
| mean anomaly at epoch: | 324.7598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|