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 24251.93155327 .00015456 00000-0 10623-2 0 9994
2 40014 98.1184 297.7662 0033968 213.8166 146.0893 15.05564701558088
| Epoch (UTC): | 07 September 2024 22:21:26 |
| Eccentricity: | 0.0033968 |
| inclination: | 98.1184° |
| perigee height: | 526 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 297.7662° |
| argument of perigee: | 213.8166° |
| revolutions per day: | 15.05564701 |
| mean anomaly at epoch: | 146.0893° |
| orbit number at epoch: | 55808 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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