View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67366U 26145.40574071 +.00000000 +00000-0 +49412-3 0 00000
2 67366 97.8017 144.3282 0007997 199.5449 160.5462 14.88038938 05
| Epoch (UTC): | 25 May 2026 09:44:15 |
| Eccentricity: | 0.0007997 |
| inclination: | 97.8017° |
| perigee height: | 598 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 144.3282° |
| argument of perigee: | 199.5449° |
| revolutions per day: | 14.88038938 |
| mean anomaly at epoch: | 160.5462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|