View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63814U 26145.55557282 +.00000000 +00000-0 +35407-3 0 00004
2 63814 43.0004 98.1538 0000707 253.9746 106.1028 15.27586791 08
| Epoch (UTC): | 25 May 2026 13:20:01 |
| Eccentricity: | 0.0000707 |
| inclination: | 43.0004° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 98.1538° |
| argument of perigee: | 253.9746° |
| revolutions per day: | 15.27586791 |
| mean anomaly at epoch: | 106.1028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|