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 37932U 11068C 25136.89071986 .00000143 00000-0 83227-4 0 9999
2 37932 98.8390 84.8820 0036060 322.5536 106.7165 14.22852054700123
| Epoch (UTC): | 16 May 2025 21:22:38 |
| Eccentricity: | 0.0036060 |
| inclination: | 98.8390° |
| perigee height: | 790 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 84.8820° |
| argument of perigee: | 322.5536° |
| revolutions per day: | 14.22852054 |
| mean anomaly at epoch: | 106.7165° |
| orbit number at epoch: | 70012 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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