View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67192U 26145.52425368 +.00000000 +00000-0 +10541-3 0 00005
2 67192 70.0015 340.7411 0002261 262.7243 97.3659 14.98333720 06
| Epoch (UTC): | 25 May 2026 12:34:55 |
| Eccentricity: | 0.0002261 |
| inclination: | 70.0015° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.7411° |
| argument of perigee: | 262.7243° |
| revolutions per day: | 14.98333720 |
| mean anomaly at epoch: | 97.3659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|