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 03093U 68002A 25193.55319272 -.00000048 00000-0 95804-4 0 9998
2 03093 105.7857 304.1190 0319382 296.9652 71.0027 12.83586678693787
| Epoch (UTC): | 12 July 2025 13:16:35 |
| Eccentricity: | 0.0319382 |
| inclination: | 105.7857° |
| perigee height: | 1081 km |
| apogee height: | 1573 km |
| right ascension of ascending node: | 304.1190° |
| argument of perigee: | 296.9652° |
| revolutions per day: | 12.83586678 |
| mean anomaly at epoch: | 71.0027° |
| orbit number at epoch: | 69378 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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