View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64575U 26145.32519707 +.00000000 +00000-0 +10016-3 0 00003
2 64575 97.7751 260.6129 0012808 15.5885 344.5727 14.94601298 08
| Epoch (UTC): | 25 May 2026 07:48:17 |
| Eccentricity: | 0.0012808 |
| inclination: | 97.7751° |
| perigee height: | 575 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 260.6129° |
| argument of perigee: | 15.5885° |
| revolutions per day: | 14.94601298 |
| mean anomaly at epoch: | 344.5727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|