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 24263.17441235 .00035465 00000-0 41486-2 0 9996
2 85 38.7308 215.0877 0242643 262.9691 94.3419 14.65492007154109
| Epoch (UTC): | 19 September 2024 04:11:09 |
| Eccentricity: | 0.0242643 |
| inclination: | 38.7308° |
| perigee height: | 504 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 215.0877° |
| argument of perigee: | 262.9691° |
| revolutions per day: | 14.65492007 |
| mean anomaly at epoch: | 94.3419° |
| orbit number at epoch: | 15410 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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