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 22279.35531880 .00014299 00000-0 27085-2 0 9998
2 85 38.7681 34.4227 0370420 5.3022 355.1496 14.28213212 50901
| Epoch (UTC): | 06 October 2022 08:31:39 |
| Eccentricity: | 0.0370420 |
| inclination: | 38.7681° |
| perigee height: | 532 km |
| apogee height: | 1063 km |
| right ascension of ascending node: | 34.4227° |
| argument of perigee: | 5.3022° |
| revolutions per day: | 14.28213212 |
| mean anomaly at epoch: | 355.1496° |
| orbit number at epoch: | 5090 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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