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 23331.89219632 .00007045 00000-0 54440-3 0 9998
2 40014 98.1517 358.4211 0036330 87.6358 272.9023 15.01336449515268
| Epoch (UTC): | 27 November 2023 21:24:45 |
| Eccentricity: | 0.0036330 |
| inclination: | 98.1517° |
| perigee height: | 537 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 358.4211° |
| argument of perigee: | 87.6358° |
| revolutions per day: | 15.01336449 |
| mean anomaly at epoch: | 272.9023° |
| orbit number at epoch: | 51526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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