View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66353U 26145.51873177 +.00000000 +00000-0 +45513-3 0 00004
2 66353 53.1588 235.2253 0001087 91.6111 268.5014 15.30202177 06
| Epoch (UTC): | 25 May 2026 12:26:58 |
| Eccentricity: | 0.0001087 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.2253° |
| argument of perigee: | 91.6111° |
| revolutions per day: | 15.30202177 |
| mean anomaly at epoch: | 268.5014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|