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 26109.23035716 +.00000000 +00000-0 +00000-0 0 00009
2 38857 55.7701 103.1616 0005947 294.3040 65.6305 1.70473325 00
| Epoch (UTC): | 19 April 2026 05:31:42 |
| Eccentricity: | 0.0005947 |
| inclination: | 55.7701° |
| perigee height: | 23205 km |
| apogee height: | 23240 km |
| right ascension of ascending node: | 103.1616° |
| argument of perigee: | 294.3040° |
| revolutions per day: | 1.70473325 |
| mean anomaly at epoch: | 65.6305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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