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 25193.65956865 .00000062 00000-0 47220-4 0 9997
2 37932 98.8413 141.8649 0037052 155.8113 16.9126 14.22868630708193
| Epoch (UTC): | 12 July 2025 15:49:46 |
| Eccentricity: | 0.0037052 |
| inclination: | 98.8413° |
| perigee height: | 789 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 141.8649° |
| argument of perigee: | 155.8113° |
| revolutions per day: | 14.22868630 |
| mean anomaly at epoch: | 16.9126° |
| orbit number at epoch: | 70819 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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