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 64588U 26145.57822797 +.00000000 +00000-0 +22623-3 0 00007
2 64588 97.7713 260.4811 0005422 71.8671 288.3139 14.94514035 02
| Epoch (UTC): | 25 May 2026 13:52:38 |
| Eccentricity: | 0.0005422 |
| inclination: | 97.7713° |
| perigee height: | 580 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 260.4811° |
| argument of perigee: | 71.8671° |
| revolutions per day: | 14.94514035 |
| mean anomaly at epoch: | 288.3139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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