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 16263U 85108B 24287.55199115 .00001720 00000-0 20022-3 0 9998
2 16263 82.5000 123.2287 0019631 168.2755 220.6954 14.84611791100982
| Epoch (UTC): | 13 October 2024 13:14:52 |
| Eccentricity: | 0.0019631 |
| inclination: | 82.5000° |
| perigee height: | 601 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 123.2287° |
| argument of perigee: | 168.2755° |
| revolutions per day: | 14.84611791 |
| mean anomaly at epoch: | 220.6954° |
| orbit number at epoch: | 10098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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