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 64520U 26145.25634521 +.00000000 +00000-0 +47815-3 0 00004
2 64520 51.9011 242.0583 0000617 94.8130 265.2903 14.79905964 00
| Epoch (UTC): | 25 May 2026 06:09:08 |
| Eccentricity: | 0.0000617 |
| inclination: | 51.9011° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 242.0583° |
| argument of perigee: | 94.8130° |
| revolutions per day: | 14.79905964 |
| mean anomaly at epoch: | 265.2903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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