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 23343.12007770 .00052699 00000-0 75826-3 0 9994
2 40910 97.4476 0.9474 0005282 182.6701 177.4526 15.55884666455896
| Epoch (UTC): | 09 December 2023 02:52:54 |
| Eccentricity: | 0.0005282 |
| inclination: | 97.4476° |
| perigee height: | 396 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 0.9474° |
| argument of perigee: | 182.6701° |
| revolutions per day: | 15.55884666 |
| mean anomaly at epoch: | 177.4526° |
| orbit number at epoch: | 45589 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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