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 25109.41618709 .00010456 00000-0 69342-3 0 9996
2 40032 98.0401 78.5324 0009183 159.9961 200.1628 15.07437439589186
| Epoch (UTC): | 19 April 2025 09:59:18 |
| Eccentricity: | 0.0009183 |
| inclination: | 98.0401° |
| perigee height: | 537 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 78.5324° |
| argument of perigee: | 159.9961° |
| revolutions per day: | 15.07437439 |
| mean anomaly at epoch: | 200.1628° |
| orbit number at epoch: | 58918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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