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 38257U 26145.63028845 +.00000000 +00000-0 +31653-3 0 00003
2 38257 97.2998 283.3753 0003516 257.1510 102.9337 15.27644959 05
| Epoch (UTC): | 25 May 2026 15:07:36 |
| Eccentricity: | 0.0003516 |
| inclination: | 97.2998° |
| perigee height: | 480 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 283.3753° |
| argument of perigee: | 257.1510° |
| revolutions per day: | 15.27644959 |
| mean anomaly at epoch: | 102.9337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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