View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46036U 26145.22498582 +.00000000 +00000-0 +20129-4 0 00008
2 46036 53.1607 131.2165 0001520 105.2740 254.8429 15.30189983 00
| Epoch (UTC): | 25 May 2026 05:23:58 |
| Eccentricity: | 0.0001520 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 131.2165° |
| argument of perigee: | 105.2740° |
| revolutions per day: | 15.30189983 |
| mean anomaly at epoch: | 254.8429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|