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 39492U 13078C 24358.24742198 .00003974 00000-0 37627-3 0 9996
2 39492 82.4169 73.9119 0016403 288.9159 71.0283 14.93304396596761
| Epoch (UTC): | 23 December 2024 05:56:17 |
| Eccentricity: | 0.0016403 |
| inclination: | 82.4169° |
| perigee height: | 576 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 73.9119° |
| argument of perigee: | 288.9159° |
| revolutions per day: | 14.93304396 |
| mean anomaly at epoch: | 71.0283° |
| orbit number at epoch: | 59676 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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