View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66759U 26145.64333503 +.00000000 +00000-0 +26913-3 0 00005
2 66759 97.4173 219.7457 0002218 64.4648 295.6817 15.20630792 09
| Epoch (UTC): | 25 May 2026 15:26:24 |
| Eccentricity: | 0.0002218 |
| inclination: | 97.4173° |
| perigee height: | 502 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 219.7457° |
| argument of perigee: | 64.4648° |
| revolutions per day: | 15.20630792 |
| mean anomaly at epoch: | 295.6817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|