View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66052U 26073.94480531 +.00000000 +00000-0 +67820-3 0 00000
2 66052 51.6276 38.9988 0003794 115.9120 244.2265 15.62833336 00
| Epoch (UTC): | 14 March 2026 22:40:31 |
| Eccentricity: | 0.0003794 |
| inclination: | 51.6276° |
| perigee height: | 377 km |
| apogee height: | 382 km |
| right ascension of ascending node: | 38.9988° |
| argument of perigee: | 115.9120° |
| revolutions per day: | 15.62833336 |
| mean anomaly at epoch: | 244.2265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|