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 38347U 26138.36816161 +.00000000 +00000-0 +25389-3 0 00000
2 38347 98.2018 269.7136 0005939 199.9559 160.1427 14.93137956 01
| Epoch (UTC): | 18 May 2026 08:50:09 |
| Eccentricity: | 0.0005939 |
| inclination: | 98.2018° |
| perigee height: | 584 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 269.7136° |
| argument of perigee: | 199.9559° |
| revolutions per day: | 14.93137956 |
| mean anomaly at epoch: | 160.1427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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