View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66291U 26145.38512943 +.00000000 +00000-0 +66932-3 0 00009
2 66291 53.1594 193.9513 0000780 71.8095 288.2993 15.34415085 06
| Epoch (UTC): | 25 May 2026 09:14:35 |
| Eccentricity: | 0.0000780 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 193.9513° |
| argument of perigee: | 71.8095° |
| revolutions per day: | 15.34415085 |
| mean anomaly at epoch: | 288.2993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|