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 23091.10067337 .00038063 00000-0 11887-2 0 9992
2 40910 97.4692 103.2236 0012180 51.3765 349.6137 15.33016211417063
| Epoch (UTC): | 01 April 2023 02:24:58 |
| Eccentricity: | 0.0012180 |
| inclination: | 97.4692° |
| perigee height: | 458 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 103.2236° |
| argument of perigee: | 51.3765° |
| revolutions per day: | 15.33016211 |
| mean anomaly at epoch: | 349.6137° |
| orbit number at epoch: | 41706 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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