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 23340.80455853 .00060781 00000-0 88216-3 0 9993
2 40910 97.4483 358.5345 0004901 193.1657 166.9470 15.55616293455538
| Epoch (UTC): | 06 December 2023 19:18:33 |
| Eccentricity: | 0.0004901 |
| inclination: | 97.4483° |
| perigee height: | 397 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 358.5345° |
| argument of perigee: | 193.1657° |
| revolutions per day: | 15.55616293 |
| mean anomaly at epoch: | 166.9470° |
| orbit number at epoch: | 45553 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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