View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63486U 26145.42161873 +.00000000 +00000-0 +56068-3 0 00008
2 63486 43.0002 186.2736 0001361 272.2708 87.7988 15.27597897 07
| Epoch (UTC): | 25 May 2026 10:07:07 |
| Eccentricity: | 0.0001361 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.2736° |
| argument of perigee: | 272.2708° |
| revolutions per day: | 15.27597897 |
| mean anomaly at epoch: | 87.7988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|