View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66736U 26145.11024385 +.00000000 +00000-0 +21625-3 0 00002
2 66736 97.4226 219.3514 0002915 50.6637 309.4857 15.20617933 02
| Epoch (UTC): | 25 May 2026 02:38:45 |
| Eccentricity: | 0.0002915 |
| inclination: | 97.4226° |
| perigee height: | 502 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 219.3514° |
| argument of perigee: | 50.6637° |
| revolutions per day: | 15.20617933 |
| mean anomaly at epoch: | 309.4857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|