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 23038.53172380 .00028928 00000-0 54265-2 0 9992
2 00085 38.7645 112.3066 0357817 123.5780 239.9664 14.30376764 68705
| Epoch (UTC): | 07 February 2023 12:45:40 |
| Eccentricity: | 0.0357817 |
| inclination: | 38.7645° |
| perigee height: | 534 km |
| apogee height: | 1047 km |
| right ascension of ascending node: | 112.3066° |
| argument of perigee: | 123.5780° |
| revolutions per day: | 14.30376764 |
| mean anomaly at epoch: | 239.9664° |
| orbit number at epoch: | 6870 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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