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 40032U 14033Y 25171.72125095 .00005078 00000-0 33005-3 0 9991
2 40032 98.0437 143.7185 0007597 334.7175 25.3679 15.08480934598050
| Epoch (UTC): | 20 June 2025 17:18:36 |
| Eccentricity: | 0.0007597 |
| inclination: | 98.0437° |
| perigee height: | 535 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 143.7185° |
| argument of perigee: | 334.7175° |
| revolutions per day: | 15.08480934 |
| mean anomaly at epoch: | 25.3679° |
| orbit number at epoch: | 59805 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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