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 41133U 00055BQ 24280.81141373 .00064261 00000-0 21674-1 0 9996
2 41133 98.9316 47.5829 0009767 192.0938 168.0014 14.36544843456665
| Epoch (UTC): | 06 October 2024 19:28:26 |
| Eccentricity: | 0.0009767 |
| inclination: | 98.9316° |
| perigee height: | 763 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 47.5829° |
| argument of perigee: | 192.0938° |
| revolutions per day: | 14.36544843 |
| mean anomaly at epoch: | 168.0014° |
| orbit number at epoch: | 45666 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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