View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65882U 26145.34868030 +.00000000 +00000-0 +60678-3 0 00002
2 65882 53.1604 14.3977 0001073 97.8131 262.2994 15.34406496 07
| Epoch (UTC): | 25 May 2026 08:22:05 |
| Eccentricity: | 0.0001073 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 14.3977° |
| argument of perigee: | 97.8131° |
| revolutions per day: | 15.34406496 |
| mean anomaly at epoch: | 262.2994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|