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 40071U 14037C 23336.90196016 .00002827 00000-0 34848-3 0 9995
2 40071 98.3423 235.4963 0009157 47.1641 313.0340 14.83745865508299
| Epoch (UTC): | 02 December 2023 21:38:49 |
| Eccentricity: | 0.0009157 |
| inclination: | 98.3423° |
| perigee height: | 611 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 235.4963° |
| argument of perigee: | 47.1641° |
| revolutions per day: | 14.83745865 |
| mean anomaly at epoch: | 313.0340° |
| orbit number at epoch: | 50829 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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