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 38176U 11068D 24357.80855568 .00006063 00000-0 15870-2 0 9995
2 38176 98.2834 0.0987 0110492 13.5168 346.8942 14.46062654683377
| Epoch (UTC): | 22 December 2024 19:24:19 |
| Eccentricity: | 0.0110492 |
| inclination: | 98.2834° |
| perigee height: | 660 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 0.0987° |
| argument of perigee: | 13.5168° |
| revolutions per day: | 14.46062654 |
| mean anomaly at epoch: | 346.8942° |
| orbit number at epoch: | 68337 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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