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 23081.25505229 .00006147 00000-0 51274-3 0 9994
2 40014 98.1459 96.3454 0029790 192.5348 167.5136 14.98637619477716
| Epoch (UTC): | 22 March 2023 06:07:16 |
| Eccentricity: | 0.0029790 |
| inclination: | 98.1459° |
| perigee height: | 550 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 96.3454° |
| argument of perigee: | 192.5348° |
| revolutions per day: | 14.98637619 |
| mean anomaly at epoch: | 167.5136° |
| orbit number at epoch: | 47771 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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