View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66360U 26145.52400985 +.00000000 +00000-0 +51631-3 0 00004
2 66360 53.1584 235.2567 0001275 91.7500 268.3647 15.30194813 07
| Epoch (UTC): | 25 May 2026 12:34:34 |
| Eccentricity: | 0.0001275 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.2567° |
| argument of perigee: | 91.7500° |
| revolutions per day: | 15.30194813 |
| mean anomaly at epoch: | 268.3647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|