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 64032U 26145.65272939 +.00000000 +00000-0 +31292-3 0 00009
2 64032 70.0003 280.2717 0002898 266.5360 93.5467 14.98338276 04
| Epoch (UTC): | 25 May 2026 15:39:55 |
| Eccentricity: | 0.0002898 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 280.2717° |
| argument of perigee: | 266.5360° |
| revolutions per day: | 14.98338276 |
| mean anomaly at epoch: | 93.5467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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