View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55923U 26145.30654328 +.00000000 +00000-0 +71204-4 0 00004
2 55923 69.9988 111.2783 0003740 267.1469 92.9262 14.98328803 03
| Epoch (UTC): | 25 May 2026 07:21:25 |
| Eccentricity: | 0.0003740 |
| inclination: | 69.9988° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 111.2783° |
| argument of perigee: | 267.1469° |
| revolutions per day: | 14.98328803 |
| mean anomaly at epoch: | 92.9262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|