View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67232U 26145.53301731 +.00000000 +00000-0 +15895-3 0 00005
2 67232 52.9941 75.3829 0012337 65.6799 294.5481 15.18385223 05
| Epoch (UTC): | 25 May 2026 12:47:32 |
| Eccentricity: | 0.0012337 |
| inclination: | 52.9941° |
| perigee height: | 502 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 75.3829° |
| argument of perigee: | 65.6799° |
| revolutions per day: | 15.18385223 |
| mean anomaly at epoch: | 294.5481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|