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 37846U 26142.03870751 +.00000000 +00000-0 +00000-0 0 00007
2 37846 57.0040 342.4699 0003643 41.9521 318.0951 1.70475642 04
| Epoch (UTC): | 22 May 2026 00:55:44 |
| Eccentricity: | 0.0003643 |
| inclination: | 57.0040° |
| perigee height: | 23211 km |
| apogee height: | 23233 km |
| right ascension of ascending node: | 342.4699° |
| argument of perigee: | 41.9521° |
| revolutions per day: | 1.70475642 |
| mean anomaly at epoch: | 318.0951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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