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 38043U 26145.52321186 +.00000000 +00000-0 -62533-4 0 00001
2 38043 52.0066 133.8835 0000241 45.5957 107.4835 12.62266873 03
| Epoch (UTC): | 25 May 2026 12:33:25 |
| Eccentricity: | 0.0000241 |
| inclination: | 52.0066° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 133.8835° |
| argument of perigee: | 45.5957° |
| revolutions per day: | 12.62266873 |
| mean anomaly at epoch: | 107.4835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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