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 01642U 65082D 24357.88920071 .00002541 00000-0 30118-3 0 9998
2 01642 32.0932 259.2373 0024179 313.6137 46.2508 14.82788996157125
| Epoch (UTC): | 22 December 2024 21:20:26 |
| Eccentricity: | 0.0024179 |
| inclination: | 32.0932° |
| perigee height: | 603 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 259.2373° |
| argument of perigee: | 313.6137° |
| revolutions per day: | 14.82788996 |
| mean anomaly at epoch: | 46.2508° |
| orbit number at epoch: | 15712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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