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 85U 61004C 23337.36490471 .00027401 00000-0 41777-2 0 9998
2 85 38.7504 344.4034 0289661 13.7679 347.0776 14.48811431111719
| Epoch (UTC): | 03 December 2023 08:45:27 |
| Eccentricity: | 0.0289661 |
| inclination: | 38.7504° |
| perigee height: | 523 km |
| apogee height: | 935 km |
| right ascension of ascending node: | 344.4034° |
| argument of perigee: | 13.7679° |
| revolutions per day: | 14.48811431 |
| mean anomaly at epoch: | 347.0776° |
| orbit number at epoch: | 11171 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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