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 55046U 23001AP 24358.11314371 .00012989 00000-0 55286-3 0 9997
2 55046 97.4017 52.7979 0009166 233.9348 126.1040 15.23085750109205
| Epoch (UTC): | 23 December 2024 02:42:55 |
| Eccentricity: | 0.0009166 |
| inclination: | 97.4017° |
| perigee height: | 490 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 52.7979° |
| argument of perigee: | 233.9348° |
| revolutions per day: | 15.23085750 |
| mean anomaly at epoch: | 126.1040° |
| orbit number at epoch: | 10920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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