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 38001U 93036BRC 24354.60101771 .00006675 00000-0 98743-3 0 9992
2 38001 74.0051 115.3910 0072544 354.0424 17.1085 14.73578476694222
| Epoch (UTC): | 19 December 2024 14:25:27 |
| Eccentricity: | 0.0072544 |
| inclination: | 74.0051° |
| perigee height: | 598 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 115.3910° |
| argument of perigee: | 354.0424° |
| revolutions per day: | 14.73578476 |
| mean anomaly at epoch: | 17.1085° |
| orbit number at epoch: | 69422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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