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 38755U 26145.49069837 +.00000000 +00000-0 +93516-4 0 00003
2 38755 98.2123 213.0640 0001310 96.0343 264.1006 14.58546891 01
| Epoch (UTC): | 25 May 2026 11:46:36 |
| Eccentricity: | 0.0001310 |
| inclination: | 98.2123° |
| perigee height: | 697 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 213.0640° |
| argument of perigee: | 96.0343° |
| revolutions per day: | 14.58546891 |
| mean anomaly at epoch: | 264.1006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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