View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67573U 26145.42635885 +.00000000 +00000-0 +77777-3 0 00008
2 67573 97.2848 205.7437 0000558 99.7920 260.3386 15.33453013 06
| Epoch (UTC): | 25 May 2026 10:13:57 |
| Eccentricity: | 0.0000558 |
| inclination: | 97.2848° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.7437° |
| argument of perigee: | 99.7920° |
| revolutions per day: | 15.33453013 |
| mean anomaly at epoch: | 260.3386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|