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 16203U 82055E 24357.90568273 .00000003 00000-0 70134-4 0 9995
2 16203 65.8327 184.4198 0077387 266.9016 208.1478 13.89127412155528
| Epoch (UTC): | 22 December 2024 21:44:10 |
| Eccentricity: | 0.0077387 |
| inclination: | 65.8327° |
| perigee height: | 875 km |
| apogee height: | 988 km |
| right ascension of ascending node: | 184.4198° |
| argument of perigee: | 266.9016° |
| revolutions per day: | 13.89127412 |
| mean anomaly at epoch: | 208.1478° |
| orbit number at epoch: | 15552 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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