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 00116U 61015A 23277.45252461 .00000070 00000-0 11249-3 0 9998
2 00116 66.8088 144.6139 0081868 246.7558 112.4886 13.91949294159356
| Epoch (UTC): | 04 October 2023 10:51:38 |
| Eccentricity: | 0.0081868 |
| inclination: | 66.8088° |
| perigee height: | 862 km |
| apogee height: | 981 km |
| right ascension of ascending node: | 144.6139° |
| argument of perigee: | 246.7558° |
| revolutions per day: | 13.91949294 |
| mean anomaly at epoch: | 112.4886° |
| orbit number at epoch: | 15935 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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