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 24262.56444316 .00009537 00000-0 65284-3 0 9991
2 40014 98.1154 308.9528 0034755 178.4803 181.6535 15.05826786559689
| Epoch (UTC): | 18 September 2024 13:32:47 |
| Eccentricity: | 0.0034755 |
| inclination: | 98.1154° |
| perigee height: | 525 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 308.9528° |
| argument of perigee: | 178.4803° |
| revolutions per day: | 15.05826786 |
| mean anomaly at epoch: | 181.6535° |
| orbit number at epoch: | 55968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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