View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67882U 26145.52905470 +.00000000 +00000-0 +45382-3 0 00009
2 67882 97.2845 79.0466 0001706 94.6743 265.4694 15.33444499 09
| Epoch (UTC): | 25 May 2026 12:41:50 |
| Eccentricity: | 0.0001706 |
| inclination: | 97.2845° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 79.0466° |
| argument of perigee: | 94.6743° |
| revolutions per day: | 15.33444499 |
| mean anomaly at epoch: | 265.4694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|