View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46585U 26145.58335647 +.00000000 +00000-0 +93013-3 0 00009
2 46585 53.0303 91.7118 0007233 81.0608 133.0415 15.90273886 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0007233 |
| inclination: | 53.0303° |
| perigee height: | 297 km |
| apogee height: | 306 km |
| right ascension of ascending node: | 91.7118° |
| argument of perigee: | 81.0608° |
| revolutions per day: | 15.90273886 |
| mean anomaly at epoch: | 133.0415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|