View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66999U 26145.14339610 +.00000000 +00000-0 +31915-3 0 00009
2 66999 97.6367 221.2823 0017274 89.9914 270.3293 15.06556150 00
| Epoch (UTC): | 25 May 2026 03:26:29 |
| Eccentricity: | 0.0017274 |
| inclination: | 97.6367° |
| perigee height: | 535 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 221.2823° |
| argument of perigee: | 89.9914° |
| revolutions per day: | 15.06556150 |
| mean anomaly at epoch: | 270.3293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|