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 26155.15303112 +.00000000 +00000-0 +37681-3 0 00004
2 38340 98.2165 287.5581 0007434 217.7503 142.3193 14.90984575 05
| Epoch (UTC): | 04 June 2026 03:40:21 |
| Eccentricity: | 0.0007434 |
| inclination: | 98.2165° |
| perigee height: | 590 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 287.5581° |
| argument of perigee: | 217.7503° |
| revolutions per day: | 14.90984575 |
| mean anomaly at epoch: | 142.3193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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