View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59166U 26143.99704878 +.00000000 +00000-0 -46189-4 0 00001
2 59166 43.0029 41.6628 0001401 262.6975 97.3718 15.27567155 06
| Epoch (UTC): | 23 May 2026 23:55:45 |
| Eccentricity: | 0.0001401 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 41.6628° |
| argument of perigee: | 262.6975° |
| revolutions per day: | 15.27567155 |
| mean anomaly at epoch: | 97.3718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|