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 38007U 26150.61630404 +.00000000 +00000-0 +19101-3 0 00004
2 38007 97.7647 147.5700 0001571 87.8623 272.2767 14.77546420 05
| Epoch (UTC): | 30 May 2026 14:47:28 |
| Eccentricity: | 0.0001571 |
| inclination: | 97.7647° |
| perigee height: | 636 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 147.5700° |
| argument of perigee: | 87.8623° |
| revolutions per day: | 14.77546420 |
| mean anomaly at epoch: | 272.2767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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