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 26032.47984498 +.00000000 +00000-0 +16977-3 0 00002
2 37794 97.8247 19.3534 0010748 238.1661 239.1566 14.65428654 08
| Epoch (UTC): | 01 February 2026 11:30:58 |
| Eccentricity: | 0.0010748 |
| inclination: | 97.8247° |
| perigee height: | 668 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 19.3534° |
| argument of perigee: | 238.1661° |
| revolutions per day: | 14.65428654 |
| mean anomaly at epoch: | 239.1566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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