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 16326U 85113A 24357.53560629 .00022394 00000-0 61552-3 0 9995
2 16326 82.4998 13.9053 0008813 122.4297 237.7801 15.37040014133345
| Epoch (UTC): | 22 December 2024 12:51:16 |
| Eccentricity: | 0.0008813 |
| inclination: | 82.4998° |
| perigee height: | 449 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 13.9053° |
| argument of perigee: | 122.4297° |
| revolutions per day: | 15.37040014 |
| mean anomaly at epoch: | 237.7801° |
| orbit number at epoch: | 13334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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