View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68178U 26145.64046476 +.00000000 +00000-0 +74805-3 0 00005
2 68178 53.1575 268.6757 0000880 89.3516 270.7587 15.34400275 04
| Epoch (UTC): | 25 May 2026 15:22:16 |
| Eccentricity: | 0.0000880 |
| inclination: | 53.1575° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 268.6757° |
| argument of perigee: | 89.3516° |
| revolutions per day: | 15.34400275 |
| mean anomaly at epoch: | 270.7587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|