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 24278.02007981 .00137495 00000-0 15462-1 0 9992
2 85 38.7237 133.6399 0231045 8.6099 351.8529 14.68036934156285
| Epoch (UTC): | 04 October 2024 00:28:54 |
| Eccentricity: | 0.0231045 |
| inclination: | 38.7237° |
| perigee height: | 504 km |
| apogee height: | 830 km |
| right ascension of ascending node: | 133.6399° |
| argument of perigee: | 8.6099° |
| revolutions per day: | 14.68036934 |
| mean anomaly at epoch: | 351.8529° |
| orbit number at epoch: | 15628 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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