View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64514U 26145.63046667 +.00000000 +00000-0 +42158-3 0 00002
2 64514 51.8974 237.8225 0000340 113.8500 246.2498 14.79945944 01
| Epoch (UTC): | 25 May 2026 15:07:52 |
| Eccentricity: | 0.0000340 |
| inclination: | 51.8974° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 237.8225° |
| argument of perigee: | 113.8500° |
| revolutions per day: | 14.79945944 |
| mean anomaly at epoch: | 246.2498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|