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 38749U 26145.42969339 +.00000000 +00000-0 +00000-0 0 00007
2 38749 0.0175 338.1781 0001965 93.4579 268.0711 1.00271812 02
| Epoch (UTC): | 25 May 2026 10:18:45 |
| Eccentricity: | 0.0001965 |
| inclination: | 0.0175° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 338.1781° |
| argument of perigee: | 93.4579° |
| revolutions per day: | 1.00271812 |
| mean anomaly at epoch: | 268.0711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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