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 42794U 26138.87396833 +.00000000 +00000-0 +19334-3 0 00009
2 42794 97.5548 117.8795 0080303 263.1857 96.0234 15.16705638 06
| Epoch (UTC): | 18 May 2026 20:58:30 |
| Eccentricity: | 0.0080303 |
| inclination: | 97.5548° |
| perigee height: | 460 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 117.8795° |
| argument of perigee: | 263.1857° |
| revolutions per day: | 15.16705638 |
| mean anomaly at epoch: | 96.0234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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