View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66993U 26145.45856170 +.00000000 +00000-0 +23572-3 0 00002
2 66993 97.6317 221.3825 0016764 78.9070 281.4041 15.06099713 07
| Epoch (UTC): | 25 May 2026 11:00:19 |
| Eccentricity: | 0.0016764 |
| inclination: | 97.6317° |
| perigee height: | 537 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 221.3825° |
| argument of perigee: | 78.9070° |
| revolutions per day: | 15.06099713 |
| mean anomaly at epoch: | 281.4041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|