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 16727U 86037A 24357.88933458 .00000115 00000-0 10625-3 0 9990
2 16727 82.9580 145.1722 0030158 273.2501 241.0288 13.74352565934806
| Epoch (UTC): | 22 December 2024 21:20:38 |
| Eccentricity: | 0.0030158 |
| inclination: | 82.9580° |
| perigee height: | 962 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 145.1722° |
| argument of perigee: | 273.2501° |
| revolutions per day: | 13.74352565 |
| mean anomaly at epoch: | 241.0288° |
| orbit number at epoch: | 93480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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