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 23090.26837460 .00006953 00000-0 57692-3 0 9995
2 40014 98.1463 105.7631 0030211 162.6395 197.5867 14.98775746479061
| Epoch (UTC): | 31 March 2023 06:26:27 |
| Eccentricity: | 0.0030211 |
| inclination: | 98.1463° |
| perigee height: | 549 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 105.7631° |
| argument of perigee: | 162.6395° |
| revolutions per day: | 14.98775746 |
| mean anomaly at epoch: | 197.5867° |
| orbit number at epoch: | 47906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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