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 40354U 14084B 24286.28339632 .16055351 16334-5 13866-3 0 9996
2 40354 74.6839 308.2656 0009245 278.5058 211.6869 16.51684655553160
| Epoch (UTC): | 12 October 2024 06:48:05 |
| Eccentricity: | 0.0009245 |
| inclination: | 74.6839° |
| perigee height: | 129 km |
| apogee height: | 141 km |
| right ascension of ascending node: | 308.2656° |
| argument of perigee: | 278.5058° |
| revolutions per day: | 16.51684655 |
| mean anomaly at epoch: | 211.6869° |
| orbit number at epoch: | 55316 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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