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 64259U 26145.38880720 +.00000000 +00000-0 +71857-3 0 00004
2 64259 53.1606 117.9805 0000932 98.4802 261.6306 15.34400421 03
| Epoch (UTC): | 25 May 2026 09:19:52 |
| Eccentricity: | 0.0000932 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 117.9805° |
| argument of perigee: | 98.4802° |
| revolutions per day: | 15.34400421 |
| mean anomaly at epoch: | 261.6306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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