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 24262.28853345 .00048954 00000-0 57213-2 0 9998
2 00085 38.7311 219.9397 0242644 256.6674 100.6927 14.65436877154013
| Epoch (UTC): | 18 September 2024 06:55:29 |
| Eccentricity: | 0.0242644 |
| inclination: | 38.7311° |
| perigee height: | 504 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 219.9397° |
| argument of perigee: | 256.6674° |
| revolutions per day: | 14.65436877 |
| mean anomaly at epoch: | 100.6927° |
| orbit number at epoch: | 15401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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