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 64582U 26145.58137566 +.00000000 +00000-0 +15615-3 0 00008
2 64582 97.7701 260.2414 0003113 82.2236 277.9336 14.91887115 00
| Epoch (UTC): | 25 May 2026 13:57:10 |
| Eccentricity: | 0.0003113 |
| inclination: | 97.7701° |
| perigee height: | 590 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 260.2414° |
| argument of perigee: | 82.2236° |
| revolutions per day: | 14.91887115 |
| mean anomaly at epoch: | 277.9336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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