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 40911U 15049N 23087.18650644 .00023593 00000-0 92929-3 0 9994
2 40911 97.4930 94.9903 0013812 84.6582 344.3166 15.25518394416002
| Epoch (UTC): | 28 March 2023 04:28:34 |
| Eccentricity: | 0.0013812 |
| inclination: | 97.4930° |
| perigee height: | 480 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 94.9903° |
| argument of perigee: | 84.6582° |
| revolutions per day: | 15.25518394 |
| mean anomaly at epoch: | 344.3166° |
| orbit number at epoch: | 41600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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