View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65933U 26145.35520575 +.00000000 +00000-0 +74696-3 0 00004
2 65933 53.1580 169.7359 0000504 22.2343 337.8681 15.33556842 03
| Epoch (UTC): | 25 May 2026 08:31:29 |
| Eccentricity: | 0.0000504 |
| inclination: | 53.1580° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 169.7359° |
| argument of perigee: | 22.2343° |
| revolutions per day: | 15.33556842 |
| mean anomaly at epoch: | 337.8681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|