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 38091U 26145.52406509 +.00000000 +00000-0 +00000-0 0 00003
2 38091 3.5199 69.8362 0010788 271.6230 149.0364 1.00274956 00
| Epoch (UTC): | 25 May 2026 12:34:39 |
| Eccentricity: | 0.0010788 |
| inclination: | 3.5199° |
| perigee height: | 35740 km |
| apogee height: | 35831 km |
| right ascension of ascending node: | 69.8362° |
| argument of perigee: | 271.6230° |
| revolutions per day: | 1.00274956 |
| mean anomaly at epoch: | 149.0364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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