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 38771U 26103.92216622 +.00000000 +00000-0 +50398-4 0 00000
2 38771 98.6569 156.6845 0002921 149.9112 210.2233 14.21430149 09
| Epoch (UTC): | 13 April 2026 22:07:55 |
| Eccentricity: | 0.0002921 |
| inclination: | 98.6569° |
| perigee height: | 818 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 156.6845° |
| argument of perigee: | 149.9112° |
| revolutions per day: | 14.21430149 |
| mean anomaly at epoch: | 210.2233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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