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 39586U 93036BUR 24356.12194535 .00001576 00000-0 71197-3 0 9999
2 39586 74.0083 147.9745 0102834 4.9914 117.5758 14.20152504559071
| Epoch (UTC): | 21 December 2024 02:55:36 |
| Eccentricity: | 0.0102834 |
| inclination: | 74.0083° |
| perigee height: | 751 km |
| apogee height: | 899 km |
| right ascension of ascending node: | 147.9745° |
| argument of perigee: | 4.9914° |
| revolutions per day: | 14.20152504 |
| mean anomaly at epoch: | 117.5758° |
| orbit number at epoch: | 55907 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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