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 43339U 18036A 25107.53885022 -.00000308 00000-0 00000+0 0 9999
2 43339 0.0166 239.3536 0000076 110.3867 184.2516 1.00269811 21027
| Epoch (UTC): | 17 April 2025 12:55:56 |
| Eccentricity: | 0.0000076 |
| inclination: | 0.0166° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 239.3536° |
| argument of perigee: | 110.3867° |
| revolutions per day: | 1.00269811 |
| mean anomaly at epoch: | 184.2516° |
| orbit number at epoch: | 2102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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