View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55615U 26145.39184939 +.00000000 +00000-0 +48203-4 0 00000
2 55615 43.0018 280.7368 0001303 274.2212 85.8491 15.27593852 03
| Epoch (UTC): | 25 May 2026 09:24:15 |
| Eccentricity: | 0.0001303 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.7368° |
| argument of perigee: | 274.2212° |
| revolutions per day: | 15.27593852 |
| mean anomaly at epoch: | 85.8491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|