View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67094U 26145.41374466 +.00000000 +00000-0 +29020-3 0 00008
2 67094 70.0009 180.8591 0004173 265.3154 94.7529 14.98345495 05
| Epoch (UTC): | 25 May 2026 09:55:47 |
| Eccentricity: | 0.0004173 |
| inclination: | 70.0009° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.8591° |
| argument of perigee: | 265.3154° |
| revolutions per day: | 14.98345495 |
| mean anomaly at epoch: | 94.7529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|