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 38045U 26145.44366794 +.00000000 +00000-0 +23636-5 0 00009
2 38045 51.9917 37.6446 0001431 25.3583 145.3897 12.62286092 04
| Epoch (UTC): | 25 May 2026 10:38:52 |
| Eccentricity: | 0.0001431 |
| inclination: | 51.9917° |
| perigee height: | 1412 km |
| apogee height: | 1415 km |
| right ascension of ascending node: | 37.6446° |
| argument of perigee: | 25.3583° |
| revolutions per day: | 12.62286092 |
| mean anomaly at epoch: | 145.3897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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