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 38857U 26143.25235125 +.00000000 +00000-0 +00000-0 0 00005
2 38857 55.7947 102.2291 0005482 300.3208 59.5856 1.70473380 03
| Epoch (UTC): | 23 May 2026 06:03:23 |
| Eccentricity: | 0.0005482 |
| inclination: | 55.7947° |
| perigee height: | 23206 km |
| apogee height: | 23238 km |
| right ascension of ascending node: | 102.2291° |
| argument of perigee: | 300.3208° |
| revolutions per day: | 1.70473380 |
| mean anomaly at epoch: | 59.5856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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