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 33591U 09005A 23340.76870805 .00000239 00000-0 15281-3 0 9992
2 33591 99.0776 29.2687 0014728 116.1484 244.1204 14.12881473764319
| Epoch (UTC): | 06 December 2023 18:26:56 |
| Eccentricity: | 0.0014728 |
| inclination: | 99.0776° |
| perigee height: | 839 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 29.2687° |
| argument of perigee: | 116.1484° |
| revolutions per day: | 14.12881473 |
| mean anomaly at epoch: | 244.1204° |
| orbit number at epoch: | 76431 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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