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 38759U 26145.58076699 +.00000000 +00000-0 +47562-3 0 00000
2 38759 64.6580 251.9328 0097061 184.3667 175.6624 15.20521942 03
| Epoch (UTC): | 25 May 2026 13:56:18 |
| Eccentricity: | 0.0097061 |
| inclination: | 64.6580° |
| perigee height: | 437 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 251.9328° |
| argument of perigee: | 184.3667° |
| revolutions per day: | 15.20521942 |
| mean anomaly at epoch: | 175.6624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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