View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43482U 26145.35284491 +.00000000 +00000-0 +76167-4 0 00009
2 43482 86.4468 97.9093 0002462 84.7155 275.4327 14.43279767 00
| Epoch (UTC): | 25 May 2026 08:28:05 |
| Eccentricity: | 0.0002462 |
| inclination: | 86.4468° |
| perigee height: | 746 km |
| apogee height: | 749 km |
| right ascension of ascending node: | 97.9093° |
| argument of perigee: | 84.7155° |
| revolutions per day: | 14.43279767 |
| mean anomaly at epoch: | 275.4327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|