View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63431U 26145.42817727 +.00000000 +00000-0 +34906-4 0 00002
2 63431 54.9896 127.6722 0002585 281.4782 78.5950 15.25120988 04
| Epoch (UTC): | 25 May 2026 10:16:34 |
| Eccentricity: | 0.0002585 |
| inclination: | 54.9896° |
| perigee height: | 489 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 127.6722° |
| argument of perigee: | 281.4782° |
| revolutions per day: | 15.25120988 |
| mean anomaly at epoch: | 78.5950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|