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 26106.62704889 +.00000000 +00000-0 +21650-3 0 00007
2 38340 98.2077 237.0957 0008496 32.3083 327.8653 14.90691040 00
| Epoch (UTC): | 16 April 2026 15:02:57 |
| Eccentricity: | 0.0008496 |
| inclination: | 98.2077° |
| perigee height: | 590 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 237.0957° |
| argument of perigee: | 32.3083° |
| revolutions per day: | 14.90691040 |
| mean anomaly at epoch: | 327.8653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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