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 12904U 81103B 24277.19134497 .00011292 00000-0 61722-3 0 9995
2 12904 81.1592 103.1600 0018723 255.5809 104.3341 15.14040865894191
| Epoch (UTC): | 03 October 2024 04:35:32 |
| Eccentricity: | 0.0018723 |
| inclination: | 81.1592° |
| perigee height: | 511 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 103.1600° |
| argument of perigee: | 255.5809° |
| revolutions per day: | 15.14040865 |
| mean anomaly at epoch: | 104.3341° |
| orbit number at epoch: | 89419 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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