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 23087.56799576 .00022863 00000-0 42842-2 0 9991
2 00085 38.7656 217.7221 0343782 96.0051 267.9980 14.32677562 75736
| Epoch (UTC): | 28 March 2023 13:37:54 |
| Eccentricity: | 0.0343782 |
| inclination: | 38.7656° |
| perigee height: | 536 km |
| apogee height: | 1029 km |
| right ascension of ascending node: | 217.7221° |
| argument of perigee: | 96.0051° |
| revolutions per day: | 14.32677562 |
| mean anomaly at epoch: | 267.9980° |
| orbit number at epoch: | 7573 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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