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 37406U 99025EFY 24275.98352084 .00006469 00000-0 38542-2 0 9993
2 37406 98.4790 172.2203 0156381 58.9926 319.5949 14.01682230571076
| Epoch (UTC): | 01 October 2024 23:36:16 |
| Eccentricity: | 0.0156381 |
| inclination: | 98.4790° |
| perigee height: | 774 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 172.2203° |
| argument of perigee: | 58.9926° |
| revolutions per day: | 14.01682230 |
| mean anomaly at epoch: | 319.5949° |
| orbit number at epoch: | 57107 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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