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 37816U 26145.58234176 +.00000000 +00000-0 +00000-0 0 00002
2 37816 0.0961 44.9387 0004061 19.8570 20.7079 1.00272549 04
| Epoch (UTC): | 25 May 2026 13:58:34 |
| Eccentricity: | 0.0004061 |
| inclination: | 0.0961° |
| perigee height: | 35769 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 44.9387° |
| argument of perigee: | 19.8570° |
| revolutions per day: | 1.00272549 |
| mean anomaly at epoch: | 20.7079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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