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 39446U 13066AG 24357.82395004 .00009565 00000-0 96848-3 0 9997
2 39446 97.8047 304.2400 0055349 319.9880 39.7266 14.90011958596753
| Epoch (UTC): | 22 December 2024 19:46:29 |
| Eccentricity: | 0.0055349 |
| inclination: | 97.8047° |
| perigee height: | 559 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 304.2400° |
| argument of perigee: | 319.9880° |
| revolutions per day: | 14.90011958 |
| mean anomaly at epoch: | 39.7266° |
| orbit number at epoch: | 59675 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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