View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67784U 26145.38218913 +.00000000 +00000-0 +22432-3 0 00004
2 67784 51.8972 218.7422 0002886 353.6800 6.4124 14.76430818 00
| Epoch (UTC): | 25 May 2026 09:10:21 |
| Eccentricity: | 0.0002886 |
| inclination: | 51.8972° |
| perigee height: | 639 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 218.7422° |
| argument of perigee: | 353.6800° |
| revolutions per day: | 14.76430818 |
| mean anomaly at epoch: | 6.4124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|