View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63895U 26145.24879688 +.00000000 +00000-0 +93817-3 0 00005
2 63895 42.9989 104.1035 0001302 273.5244 86.5458 15.27590663 01
| Epoch (UTC): | 25 May 2026 05:58:16 |
| Eccentricity: | 0.0001302 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.1035° |
| argument of perigee: | 273.5244° |
| revolutions per day: | 15.27590663 |
| mean anomaly at epoch: | 86.5458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|