View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66074U 26145.01477958 +.00000000 +00000-0 +86672-3 0 00007
2 66074 53.1602 250.9986 0001202 84.9427 275.1711 15.30208186 08
| Epoch (UTC): | 25 May 2026 00:21:16 |
| Eccentricity: | 0.0001202 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 250.9986° |
| argument of perigee: | 84.9427° |
| revolutions per day: | 15.30208186 |
| mean anomaly at epoch: | 275.1711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|