View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67590U 26145.61107245 +.00000000 +00000-0 +71268-3 0 00001
2 67590 97.2847 210.7476 0000693 104.0132 256.1188 15.33449501 08
| Epoch (UTC): | 25 May 2026 14:39:56 |
| Eccentricity: | 0.0000693 |
| inclination: | 97.2847° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.7476° |
| argument of perigee: | 104.0132° |
| revolutions per day: | 15.33449501 |
| mean anomaly at epoch: | 256.1188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|