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 38040U 26145.56664064 +.00000000 +00000-0 +69751-4 0 00005
2 38040 52.0009 86.1453 0000786 51.0688 120.2834 12.62267205 02
| Epoch (UTC): | 25 May 2026 13:35:57 |
| Eccentricity: | 0.0000786 |
| inclination: | 52.0009° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 86.1453° |
| argument of perigee: | 51.0688° |
| revolutions per day: | 12.62267205 |
| mean anomaly at epoch: | 120.2834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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