View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67790U 26145.58335647 +.00000000 +00000-0 -40761-2 0 00002
2 67790 51.8983 210.9483 0005075 17.8327 302.4246 14.92751062 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005075 |
| inclination: | 51.8983° |
| perigee height: | 586 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 210.9483° |
| argument of perigee: | 17.8327° |
| revolutions per day: | 14.92751062 |
| mean anomaly at epoch: | 302.4246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|