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 23027.42868243 .00010653 00000-0 20178-2 0 9990
2 85 38.7657 169.8125 0359926 48.4832 314.6221 14.30016279 67089
| Epoch (UTC): | 27 January 2023 10:17:18 |
| Eccentricity: | 0.0359926 |
| inclination: | 38.7657° |
| perigee height: | 533 km |
| apogee height: | 1050 km |
| right ascension of ascending node: | 169.8125° |
| argument of perigee: | 48.4832° |
| revolutions per day: | 14.30016279 |
| mean anomaly at epoch: | 314.6221° |
| orbit number at epoch: | 6708 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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