View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32376U 07059A 23147.80704429 .00000486 00000-0 67662-4 0 9992
2 32376 97.8886 331.5789 0001305 92.3392 267.7970 14.82157837836711
| Epoch (UTC): | 27 May 2023 19:22:08 |
| Eccentricity: | 0.0001305 |
| inclination: | 97.8886° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 331.5789° |
| argument of perigee: | 92.3392° |
| revolutions per day: | 14.82157837 |
| mean anomaly at epoch: | 267.7970° |
| orbit number at epoch: | 83671 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|