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 24247.22247623 .00047886 00000-0 57481-2 0 9991
2 00085 38.7314 302.3767 0244110 149.3688 212.1579 14.64243578151806
| Epoch (UTC): | 03 September 2024 05:20:21 |
| Eccentricity: | 0.0244110 |
| inclination: | 38.7314° |
| perigee height: | 507 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 302.3767° |
| argument of perigee: | 149.3688° |
| revolutions per day: | 14.64243578 |
| mean anomaly at epoch: | 212.1579° |
| orbit number at epoch: | 15180 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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