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 64882U 26145.58808677 +.00000000 +00000-0 +31815-3 0 00009
2 64882 97.4566 114.0496 0005199 253.6792 106.3877 15.29080200 09
| Epoch (UTC): | 25 May 2026 14:06:50 |
| Eccentricity: | 0.0005199 |
| inclination: | 97.4566° |
| perigee height: | 475 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 114.0496° |
| argument of perigee: | 253.6792° |
| revolutions per day: | 15.29080200 |
| mean anomaly at epoch: | 106.3877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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