View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56146U 26145.08568830 +.00000000 +00000-0 +22448-4 0 00005
2 56146 43.0050 75.5588 0001374 263.1095 96.9601 15.27578257 05
| Epoch (UTC): | 25 May 2026 02:03:23 |
| Eccentricity: | 0.0001374 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 75.5588° |
| argument of perigee: | 263.1095° |
| revolutions per day: | 15.27578257 |
| mean anomaly at epoch: | 96.9601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|