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 37393U 26145.59412847 +.00000000 +00000-0 +00000-0 0 00006
2 37393 0.0126 324.4404 0003305 111.2312 73.8879 1.00270541 01
| Epoch (UTC): | 25 May 2026 14:15:32 |
| Eccentricity: | 0.0003305 |
| inclination: | 0.0126° |
| perigee height: | 35773 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 324.4404° |
| argument of perigee: | 111.2312° |
| revolutions per day: | 1.00270541 |
| mean anomaly at epoch: | 73.8879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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