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 38011U 26088.16763093 +.00000000 +00000-0 +17195-3 0 00001
2 38011 97.8152 150.4540 0001663 85.5040 359.0019 14.82326324 06
| Epoch (UTC): | 29 March 2026 04:01:23 |
| Eccentricity: | 0.0001663 |
| inclination: | 97.8152° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 150.4540° |
| argument of perigee: | 85.5040° |
| revolutions per day: | 14.82326324 |
| mean anomaly at epoch: | 359.0019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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