View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 39443U 13066AD 24275.79969039 .13323254 25297-5 21908-2 0 9996
2 39443 97.3466 290.9212 0010565 220.7801 139.2705 16.33334340592252
| Epoch (UTC): | 01 October 2024 19:11:33 |
| Eccentricity: | 0.0010565 |
| inclination: | 97.3466° |
| perigee height: | 176 km |
| apogee height: | 190 km |
| right ascension of ascending node: | 290.9212° |
| argument of perigee: | 220.7801° |
| revolutions per day: | 16.33334340 |
| mean anomaly at epoch: | 139.2705° |
| orbit number at epoch: | 59225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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