View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39161U 13021C 24280.99584517 .00010101 00000-0 14209-2 0 9992
2 39161 97.8164 344.0615 0008093 221.1160 138.9441 14.77506766613631
| Epoch (UTC): | 06 October 2024 23:54:01 |
| Eccentricity: | 0.0008093 |
| inclination: | 97.8164° |
| perigee height: | 631 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 344.0615° |
| argument of perigee: | 221.1160° |
| revolutions per day: | 14.77506766 |
| mean anomaly at epoch: | 138.9441° |
| orbit number at epoch: | 61363 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|