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 40381U 15004A 23263.88637868 0.00000000 00000-0 00000-0 0 09
2 40381 97.4759 325.6716 0004376 332.2237 27.5501 15.17630005 09
| Epoch (UTC): | 20 September 2023 21:16:23 |
| Eccentricity: | 0.0004376 |
| inclination: | 97.4759° |
| perigee height: | 510 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 325.6716° |
| argument of perigee: | 332.2237° |
| revolutions per day: | 15.17630005 |
| mean anomaly at epoch: | 27.5501° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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