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 37386U 11014A 24354.72868504 0.00000000 00000-0 00000-0 0 05
2 37386 63.4295 231.2503 0304583 356.1656 3.8344 13.40950214 00
| Epoch (UTC): | 19 December 2024 17:29:18 |
| Eccentricity: | 0.0304583 |
| inclination: | 63.4295° |
| perigee height: | 878 km |
| apogee height: | 1333 km |
| right ascension of ascending node: | 231.2503° |
| argument of perigee: | 356.1656° |
| revolutions per day: | 13.40950214 |
| mean anomaly at epoch: | 3.8344° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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