View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66650U 26145.36407299 +.00000000 +00000-0 +27615-3 0 00008
2 66650 97.7480 74.7846 0013594 72.3786 287.8917 14.92784336 00
| Epoch (UTC): | 25 May 2026 08:44:15 |
| Eccentricity: | 0.0013594 |
| inclination: | 97.7480° |
| perigee height: | 580 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 74.7846° |
| argument of perigee: | 72.3786° |
| revolutions per day: | 14.92784336 |
| mean anomaly at epoch: | 287.8917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|