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 37794U 26130.23114786 +.00000000 +00000-0 +85173-4 0 00005
2 37794 97.8361 112.5304 0010675 294.0918 76.4760 14.65598190 02
| Epoch (UTC): | 10 May 2026 05:32:51 |
| Eccentricity: | 0.0010675 |
| inclination: | 97.8361° |
| perigee height: | 668 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 112.5304° |
| argument of perigee: | 294.0918° |
| revolutions per day: | 14.65598190 |
| mean anomaly at epoch: | 76.4760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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