View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67111U 26145.55477332 +.00000000 +00000-0 +86754-3 0 00006
2 67111 42.9988 94.7262 0002352 276.6327 83.4256 15.27622360 05
| Epoch (UTC): | 25 May 2026 13:18:52 |
| Eccentricity: | 0.0002352 |
| inclination: | 42.9988° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 94.7262° |
| argument of perigee: | 276.6327° |
| revolutions per day: | 15.27622360 |
| mean anomaly at epoch: | 83.4256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|