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 27433U 02024D 23271.66831053 .00000617 00000-0 35422-3 0 9997
2 27433 99.0457 299.3516 0015426 72.0663 288.2189 14.13133944101061
| Epoch (UTC): | 28 September 2023 16:02:22 |
| Eccentricity: | 0.0015426 |
| inclination: | 99.0457° |
| perigee height: | 837 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 299.3516° |
| argument of perigee: | 72.0663° |
| revolutions per day: | 14.13133944 |
| mean anomaly at epoch: | 288.2189° |
| orbit number at epoch: | 10106 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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