View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67239U 26145.39903602 +.00000000 +00000-0 +66316-4 0 00006
2 67239 50.0035 197.8065 0001045 249.1273 110.9487 13.29322420 04
| Epoch (UTC): | 25 May 2026 09:34:36 |
| Eccentricity: | 0.0001045 |
| inclination: | 50.0035° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 197.8065° |
| argument of perigee: | 249.1273° |
| revolutions per day: | 13.29322420 |
| mean anomaly at epoch: | 110.9487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|