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 38339U 26145.60428560 +.00000000 +00000-0 +86789-4 0 00000
2 38339 98.1350 241.3836 0007269 21.1152 339.0356 14.75776436 06
| Epoch (UTC): | 25 May 2026 14:30:10 |
| Eccentricity: | 0.0007269 |
| inclination: | 98.1350° |
| perigee height: | 638 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 241.3836° |
| argument of perigee: | 21.1152° |
| revolutions per day: | 14.75776436 |
| mean anomaly at epoch: | 339.0356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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