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 38093U 26145.40315318 +.00000000 +00000-0 +00000-0 0 00009
2 38093 5.4304 47.1689 0059161 0.0986 240.9359 1.00271573 09
| Epoch (UTC): | 25 May 2026 09:40:32 |
| Eccentricity: | 0.0059161 |
| inclination: | 5.4304° |
| perigee height: | 35537 km |
| apogee height: | 36036 km |
| right ascension of ascending node: | 47.1689° |
| argument of perigee: | 0.0986° |
| revolutions per day: | 1.00271573 |
| mean anomaly at epoch: | 240.9359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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