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 28385U 04034B 24281.33702927 .00643495 69894-5 16440-2 0 9996
2 28385 57.1255 34.7653 0956539 78.6473 292.0304 14.01447304203747
| Epoch (UTC): | 07 October 2024 08:05:19 |
| Eccentricity: | 0.0956539 |
| inclination: | 57.1255° |
| perigee height: | 193 km |
| apogee height: | 1584 km |
| right ascension of ascending node: | 34.7653° |
| argument of perigee: | 78.6473° |
| revolutions per day: | 14.01447304 |
| mean anomaly at epoch: | 292.0304° |
| orbit number at epoch: | 20374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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