View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66581U 26145.66075074 +.00000000 +00000-0 +57560-3 0 00008
2 66581 43.0011 272.1785 0000673 283.3210 76.7566 15.27598639 06
| Epoch (UTC): | 25 May 2026 15:51:28 |
| Eccentricity: | 0.0000673 |
| inclination: | 43.0011° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 272.1785° |
| argument of perigee: | 283.3210° |
| revolutions per day: | 15.27598639 |
| mean anomaly at epoch: | 76.7566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|