View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66776U 26145.46024053 +.00000000 +00000-0 +24789-3 0 00000
2 66776 97.4179 219.6880 0000683 147.0721 213.0558 15.20975697 09
| Epoch (UTC): | 25 May 2026 11:02:44 |
| Eccentricity: | 0.0000683 |
| inclination: | 97.4179° |
| perigee height: | 502 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 219.6880° |
| argument of perigee: | 147.0721° |
| revolutions per day: | 15.20975697 |
| mean anomaly at epoch: | 213.0558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|