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 40910U 15049M 23275.81841198 .00064640 00000-0 13170-2 0 9996
2 40910 97.4574 291.2981 0010479 97.5386 262.7054 15.45963376445461
| Epoch (UTC): | 02 October 2023 19:38:30 |
| Eccentricity: | 0.0010479 |
| inclination: | 97.4574° |
| perigee height: | 421 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 291.2981° |
| argument of perigee: | 97.5386° |
| revolutions per day: | 15.45963376 |
| mean anomaly at epoch: | 262.7054° |
| orbit number at epoch: | 44546 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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