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 38070U 26146.10023388 +.00000000 +00000-0 +00000-0 0 00005
2 38070 0.0167 310.2542 0000937 346.2893 71.6323 1.00267425 04
| Epoch (UTC): | 26 May 2026 02:24:20 |
| Eccentricity: | 0.0000937 |
| inclination: | 0.0167° |
| perigee height: | 35784 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 310.2542° |
| argument of perigee: | 346.2893° |
| revolutions per day: | 1.00267425 |
| mean anomaly at epoch: | 71.6323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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