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 38340U 26159.85073306 +.00000000 +00000-0 +39169-3 0 00007
2 38340 98.2164 292.4474 0007700 200.4450 159.6460 14.91018765 04
| Epoch (UTC): | 08 June 2026 20:25:03 |
| Eccentricity: | 0.0007700 |
| inclination: | 98.2164° |
| perigee height: | 589 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 292.4474° |
| argument of perigee: | 200.4450° |
| revolutions per day: | 14.91018765 |
| mean anomaly at epoch: | 159.6460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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