View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61018U 26145.56226278 +.00000000 +00000-0 +17905-3 0 00000
2 61018 50.0040 188.0114 0027865 5.5459 354.5783 14.84140173 04
| Epoch (UTC): | 25 May 2026 13:29:39 |
| Eccentricity: | 0.0027865 |
| inclination: | 50.0040° |
| perigee height: | 597 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 188.0114° |
| argument of perigee: | 5.5459° |
| revolutions per day: | 14.84140173 |
| mean anomaly at epoch: | 354.5783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|