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 23037.39056919 .00000087 00000-0 12585-3 0 9997
2 00116 66.8113 11.6217 0070497 49.7906 310.9314 13.91876002125944
| Epoch (UTC): | 06 February 2023 09:22:25 |
| Eccentricity: | 0.0070497 |
| inclination: | 66.8113° |
| perigee height: | 870 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 11.6217° |
| argument of perigee: | 49.7906° |
| revolutions per day: | 13.91876002 |
| mean anomaly at epoch: | 310.9314° |
| orbit number at epoch: | 12594 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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