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 24255.06373732 .00035160 00000-0 41690-2 0 9990
2 85 38.7318 259.4910 0243840 205.3357 153.5274 14.64822994152915
| Epoch (UTC): | 11 September 2024 01:31:46 |
| Eccentricity: | 0.0243840 |
| inclination: | 38.7318° |
| perigee height: | 505 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 259.4910° |
| argument of perigee: | 205.3357° |
| revolutions per day: | 14.64822994 |
| mean anomaly at epoch: | 153.5274° |
| orbit number at epoch: | 15291 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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