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 00085U 61004C 23084.70984381 .00018930 00000-0 35502-2 0 9999
2 00085 38.7647 232.5753 0344720 76.5710 287.3215 14.32560724 75322
| Epoch (UTC): | 25 March 2023 17:02:10 |
| Eccentricity: | 0.0344720 |
| inclination: | 38.7647° |
| perigee height: | 536 km |
| apogee height: | 1030 km |
| right ascension of ascending node: | 232.5753° |
| argument of perigee: | 76.5710° |
| revolutions per day: | 14.32560724 |
| mean anomaly at epoch: | 287.3215° |
| orbit number at epoch: | 7532 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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