View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68633U 26145.31023176 +.00000000 +00000-0 +37805-3 0 00006
2 68633 60.0219 265.6350 0025195 15.7471 344.4388 15.25642100 00
| Epoch (UTC): | 25 May 2026 07:26:44 |
| Eccentricity: | 0.0025195 |
| inclination: | 60.0219° |
| perigee height: | 472 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 265.6350° |
| argument of perigee: | 15.7471° |
| revolutions per day: | 15.25642100 |
| mean anomaly at epoch: | 344.4388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|