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 38860U 26145.59852076 +.00000000 +00000-0 +11846-3 0 00001
2 38860 97.6695 118.3704 0024907 335.1744 24.8271 14.85419646 04
| Epoch (UTC): | 25 May 2026 14:21:52 |
| Eccentricity: | 0.0024907 |
| inclination: | 97.6695° |
| perigee height: | 595 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 118.3704° |
| argument of perigee: | 335.1744° |
| revolutions per day: | 14.85419646 |
| mean anomaly at epoch: | 24.8271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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