View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66210U 26145.24425801 +.00000000 +00000-0 +83407-3 0 00007
2 66210 53.1591 234.0920 0001128 83.0002 277.1127 15.30215866 00
| Epoch (UTC): | 25 May 2026 05:51:43 |
| Eccentricity: | 0.0001128 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 234.0920° |
| argument of perigee: | 83.0002° |
| revolutions per day: | 15.30215866 |
| mean anomaly at epoch: | 277.1127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|