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 37839U 26032.37323133 +.00000000 +00000-0 +11992-3 0 00006
2 37839 19.9617 53.5149 0018642 17.2457 121.0336 14.13723833 00
| Epoch (UTC): | 01 February 2026 08:57:27 |
| Eccentricity: | 0.0018642 |
| inclination: | 19.9617° |
| perigee height: | 833 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 53.5149° |
| argument of perigee: | 17.2457° |
| revolutions per day: | 14.13723833 |
| mean anomaly at epoch: | 121.0336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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