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 40912U 15049P 23087.23717917 .00051249 00000-0 13830-2 0 9990
2 40912 97.4254 103.7612 0010027 28.4662 36.9750 15.37563118417144
| Epoch (UTC): | 28 March 2023 05:41:32 |
| Eccentricity: | 0.0010027 |
| inclination: | 97.4254° |
| perigee height: | 446 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 103.7612° |
| argument of perigee: | 28.4662° |
| revolutions per day: | 15.37563118 |
| mean anomaly at epoch: | 36.9750° |
| orbit number at epoch: | 41714 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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