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 37793U 26145.53981806 +.00000000 +00000-0 +84752-4 0 00000
2 37793 98.2379 55.5760 0043591 156.7472 19.2501 14.76878118 00
| Epoch (UTC): | 25 May 2026 12:57:20 |
| Eccentricity: | 0.0043591 |
| inclination: | 98.2379° |
| perigee height: | 609 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 55.5760° |
| argument of perigee: | 156.7472° |
| revolutions per day: | 14.76878118 |
| mean anomaly at epoch: | 19.2501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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