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 14781U 84021B 24284.48548239 .00005199 00000-0 57674-3 0 9995
2 14781 97.7207 250.4404 0009742 62.6176 297.6031 14.87636201165620
| Epoch (UTC): | 10 October 2024 11:39:05 |
| Eccentricity: | 0.0009742 |
| inclination: | 97.7207° |
| perigee height: | 598 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 250.4404° |
| argument of perigee: | 62.6176° |
| revolutions per day: | 14.87636201 |
| mean anomaly at epoch: | 297.6031° |
| orbit number at epoch: | 16562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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