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 64932U 26145.58826420 +.00000000 +00000-0 +37175-3 0 00006
2 64932 97.4500 9.4368 0002177 85.2615 274.8860 15.05659409 04
| Epoch (UTC): | 25 May 2026 14:07:06 |
| Eccentricity: | 0.0002177 |
| inclination: | 97.4500° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.4368° |
| argument of perigee: | 85.2615° |
| revolutions per day: | 15.05659409 |
| mean anomaly at epoch: | 274.8860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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