View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64839U 26145.58335647 +.00000000 +00000-0 -26241-2 0 00000
2 64839 51.8906 268.9380 0003457 190.9180 248.1606 14.97647977 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003457 |
| inclination: | 51.8906° |
| perigee height: | 572 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 268.9380° |
| argument of perigee: | 190.9180° |
| revolutions per day: | 14.97647977 |
| mean anomaly at epoch: | 248.1606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|