View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63591U 26145.32545760 +.00000000 +00000-0 +97232-3 0 00003
2 63591 43.0002 248.6492 0000563 10.5259 349.5604 15.27603434 02
| Epoch (UTC): | 25 May 2026 07:48:39 |
| Eccentricity: | 0.0000563 |
| inclination: | 43.0002° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 248.6492° |
| argument of perigee: | 10.5259° |
| revolutions per day: | 15.27603434 |
| mean anomaly at epoch: | 349.5604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|