View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32785U 26039.85210095 +.00000000 +00000-0 +42665-3 0 00004
2 32785 97.8166 18.8281 0011306 102.4524 257.7969 15.07942202 08
| Epoch (UTC): | 08 February 2026 20:27:01 |
| Eccentricity: | 0.0011306 |
| inclination: | 97.8166° |
| perigee height: | 535 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 18.8281° |
| argument of perigee: | 102.4524° |
| revolutions per day: | 15.07942202 |
| mean anomaly at epoch: | 257.7969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|