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 40014U 14033E 23087.59784124 .00008007 00000-0 66403-3 0 9997
2 40014 98.1456 102.9738 0030265 171.1169 189.0580 14.98742347478667
| Epoch (UTC): | 28 March 2023 14:20:53 |
| Eccentricity: | 0.0030265 |
| inclination: | 98.1456° |
| perigee height: | 550 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 102.9738° |
| argument of perigee: | 171.1169° |
| revolutions per day: | 14.98742347 |
| mean anomaly at epoch: | 189.0580° |
| orbit number at epoch: | 47866 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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