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 37746U 26109.02265177 +.00000000 +00000-0 +00000-0 0 00008
2 37746 5.1480 76.8005 0005152 185.0065 30.6510 0.98856863 09
| Epoch (UTC): | 19 April 2026 00:32:37 |
| Eccentricity: | 0.0005152 |
| inclination: | 5.1480° |
| perigee height: | 36166 km |
| apogee height: | 36210 km |
| right ascension of ascending node: | 76.8005° |
| argument of perigee: | 185.0065° |
| revolutions per day: | 0.98856863 |
| mean anomaly at epoch: | 30.6510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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