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 23038.39654537 .00000115 00000-0 14769-3 0 9996
2 00116 66.8114 9.1621 0070558 49.0290 311.6865 13.91876511126083
| Epoch (UTC): | 07 February 2023 09:31:01 |
| Eccentricity: | 0.0070558 |
| inclination: | 66.8114° |
| perigee height: | 870 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 9.1621° |
| argument of perigee: | 49.0290° |
| revolutions per day: | 13.91876511 |
| mean anomaly at epoch: | 311.6865° |
| orbit number at epoch: | 12608 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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