View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64771U 26145.57040584 +.00000000 +00000-0 +35740-3 0 00001
2 64771 53.1593 244.8580 0001096 344.5277 15.5692 15.34387190 01
| Epoch (UTC): | 25 May 2026 13:41:23 |
| Eccentricity: | 0.0001096 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 244.8580° |
| argument of perigee: | 344.5277° |
| revolutions per day: | 15.34387190 |
| mean anomaly at epoch: | 15.5692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|