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 36272U 99025DWZ 24352.33873390 .00001948 00000-0 87316-3 0 9997
2 36272 99.1829 211.7464 0170187 207.0691 152.1530 14.16313071585130
| Epoch (UTC): | 17 December 2024 08:07:46 |
| Eccentricity: | 0.0170187 |
| inclination: | 99.1829° |
| perigee height: | 715 km |
| apogee height: | 960 km |
| right ascension of ascending node: | 211.7464° |
| argument of perigee: | 207.0691° |
| revolutions per day: | 14.16313071 |
| mean anomaly at epoch: | 152.1530° |
| orbit number at epoch: | 58513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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