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 68371U 26145.10487744 +.00000000 +00000-0 +35165-3 0 00004
2 68371 82.2927 38.6752 0003122 282.2576 77.8331 15.61626082 04
| Epoch (UTC): | 25 May 2026 02:31:01 |
| Eccentricity: | 0.0003122 |
| inclination: | 82.2927° |
| perigee height: | 381 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 38.6752° |
| argument of perigee: | 282.2576° |
| revolutions per day: | 15.61626082 |
| mean anomaly at epoch: | 77.8331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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