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 38733U 26145.58834073 +.00000000 +00000-0 +61466-3 0 00009
2 38733 82.4731 89.3156 0019613 122.3900 237.9081 12.42434439 06
| Epoch (UTC): | 25 May 2026 14:07:12 |
| Eccentricity: | 0.0019613 |
| inclination: | 82.4731° |
| perigee height: | 1481 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 89.3156° |
| argument of perigee: | 122.3900° |
| revolutions per day: | 12.42434439 |
| mean anomaly at epoch: | 237.9081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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