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 23337.08916341 .00023786 00000-0 36319-2 0 9994
2 85 38.7504 345.8739 0289684 11.8410 348.8978 14.48791155111671
| Epoch (UTC): | 03 December 2023 02:08:23 |
| Eccentricity: | 0.0289684 |
| inclination: | 38.7504° |
| perigee height: | 524 km |
| apogee height: | 935 km |
| right ascension of ascending node: | 345.8739° |
| argument of perigee: | 11.8410° |
| revolutions per day: | 14.48791155 |
| mean anomaly at epoch: | 348.8978° |
| orbit number at epoch: | 11167 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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