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 15071U 84065C 23246.91411770 0.00004500 00000-0 38636-3 0 05
2 15071 95.9119 339.0357 0002485 313.0143 46.9855 14.97545737 03
| Epoch (UTC): | 03 September 2023 21:56:19 |
| Eccentricity: | 0.0002485 |
| inclination: | 95.9119° |
| perigee height: | 573 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 339.0357° |
| argument of perigee: | 313.0143° |
| revolutions per day: | 14.97545737 |
| mean anomaly at epoch: | 46.9855° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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