View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68764U 26145.60294713 +.00000000 +00000-0 +15771-3 0 00008
2 68764 97.7745 282.6357 0007724 94.3722 265.8387 15.05667932 05
| Epoch (UTC): | 25 May 2026 14:28:14 |
| Eccentricity: | 0.0007724 |
| inclination: | 97.7745° |
| perigee height: | 544 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 282.6357° |
| argument of perigee: | 94.3722° |
| revolutions per day: | 15.05667932 |
| mean anomaly at epoch: | 265.8387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|