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 28352U 04021A 24340.85114493 -.00000004 00000-0 23504-4 0 9998
2 28352 71.0070 186.2249 0010853 276.3956 83.5929 14.12057654 55948
| Epoch (UTC): | 05 December 2024 20:25:38 |
| Eccentricity: | 0.0010853 |
| inclination: | 71.0070° |
| perigee height: | 844 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 186.2249° |
| argument of perigee: | 276.3956° |
| revolutions per day: | 14.12057654 |
| mean anomaly at epoch: | 83.5929° |
| orbit number at epoch: | 5594 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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