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 23271.89232402 .00005896 00000-0 46768-3 0 9997
2 40014 98.1416 295.5400 0033628 288.6691 71.0882 15.00497565506264
| Epoch (UTC): | 28 September 2023 21:24:56 |
| Eccentricity: | 0.0033628 |
| inclination: | 98.1416° |
| perigee height: | 542 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 295.5400° |
| argument of perigee: | 288.6691° |
| revolutions per day: | 15.00497565 |
| mean anomaly at epoch: | 71.0882° |
| orbit number at epoch: | 50626 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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