View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55371U 26145.56260532 +.00000000 +00000-0 +87982-4 0 00009
2 55371 43.0011 247.0720 0001113 275.4761 84.5963 15.27573184 00
| Epoch (UTC): | 25 May 2026 13:30:09 |
| Eccentricity: | 0.0001113 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.0720° |
| argument of perigee: | 275.4761° |
| revolutions per day: | 15.27573184 |
| mean anomaly at epoch: | 84.5963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|