View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64547U 26145.54532932 +.00000000 +00000-0 +32547-3 0 00004
2 64547 97.4598 261.4027 0000868 77.2232 282.9103 15.24698275 01
| Epoch (UTC): | 25 May 2026 13:05:16 |
| Eccentricity: | 0.0000868 |
| inclination: | 97.4598° |
| perigee height: | 491 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 261.4027° |
| argument of perigee: | 77.2232° |
| revolutions per day: | 15.24698275 |
| mean anomaly at epoch: | 282.9103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|