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 38331U 26145.39445065 +.00000000 +00000-0 +00000-0 0 00005
2 38331 0.0382 111.2659 0002570 320.7594 76.9693 1.00271181 03
| Epoch (UTC): | 25 May 2026 09:28:00 |
| Eccentricity: | 0.0002570 |
| inclination: | 0.0382° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 111.2659° |
| argument of perigee: | 320.7594° |
| revolutions per day: | 1.00271181 |
| mean anomaly at epoch: | 76.9693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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