View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63288U 26145.51942046 +.00000000 +00000-0 +18132-3 0 00007
2 63288 82.4925 92.7501 0025778 83.9872 276.4144 12.42866371 07
| Epoch (UTC): | 25 May 2026 12:27:57 |
| Eccentricity: | 0.0025778 |
| inclination: | 82.4925° |
| perigee height: | 1474 km |
| apogee height: | 1515 km |
| right ascension of ascending node: | 92.7501° |
| argument of perigee: | 83.9872° |
| revolutions per day: | 12.42866371 |
| mean anomaly at epoch: | 276.4144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|