View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67195U 26145.29060593 +.00000000 +00000-0 +16300-3 0 00006
2 67195 70.0021 341.5227 0002834 265.8715 94.2120 14.98337675 06
| Epoch (UTC): | 25 May 2026 06:58:28 |
| Eccentricity: | 0.0002834 |
| inclination: | 70.0021° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.5227° |
| argument of perigee: | 265.8715° |
| revolutions per day: | 14.98337675 |
| mean anomaly at epoch: | 94.2120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|