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 116U 61015A 23270.84215226 .00000081 00000-0 12082-3 0 9990
2 116 66.8095 160.7786 0082117 251.0569 108.1597 13.91947273158939
| Epoch (UTC): | 27 September 2023 20:12:41 |
| Eccentricity: | 0.0082117 |
| inclination: | 66.8095° |
| perigee height: | 862 km |
| apogee height: | 982 km |
| right ascension of ascending node: | 160.7786° |
| argument of perigee: | 251.0569° |
| revolutions per day: | 13.91947273 |
| mean anomaly at epoch: | 108.1597° |
| orbit number at epoch: | 15893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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