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 23030.34872824 .00000027 00000-0 79552-4 0 9998
2 00116 66.8104 28.8388 0070110 55.1101 305.6541 13.91873846124960
| Epoch (UTC): | 30 January 2023 08:22:10 |
| Eccentricity: | 0.0070110 |
| inclination: | 66.8104° |
| perigee height: | 871 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 28.8388° |
| argument of perigee: | 55.1101° |
| revolutions per day: | 13.91873846 |
| mean anomaly at epoch: | 305.6541° |
| orbit number at epoch: | 12496 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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