View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64039U 26145.64040127 +.00000000 +00000-0 +96927-4 0 00004
2 64039 70.0010 280.6284 0002755 263.8071 96.2775 14.98342596 05
| Epoch (UTC): | 25 May 2026 15:22:10 |
| Eccentricity: | 0.0002755 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 280.6284° |
| argument of perigee: | 263.8071° |
| revolutions per day: | 14.98342596 |
| mean anomaly at epoch: | 96.2775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|