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 is defined by the following mean orbital elements,
1 37388U 26145.43665751 +.00000000 +00000-0 +89384-4 0 00003
2 37388 98.3670 120.5187 0015511 51.7628 112.8705 14.25619222 08
| Epoch (UTC): | 25 May 2026 10:28:47 |
| Eccentricity: | 0.0015511 |
| inclination: | 98.3670° |
| perigee height: | 795 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 120.5187° |
| argument of perigee: | 51.7628° |
| revolutions per day: | 14.25619222 |
| mean anomaly at epoch: | 112.8705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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