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 38711U 26145.58517875 +.00000000 +00000-0 +72118-4 0 00000
2 38711 98.9692 262.1121 0010668 229.9409 130.0834 14.25418919 09
| Epoch (UTC): | 25 May 2026 14:02:39 |
| Eccentricity: | 0.0010668 |
| inclination: | 98.9692° |
| perigee height: | 799 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 262.1121° |
| argument of perigee: | 229.9409° |
| revolutions per day: | 14.25418919 |
| mean anomaly at epoch: | 130.0834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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