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 64719U 26145.62584740 +.00000000 +00000-0 +26698-3 0 00008
2 64719 70.0003 120.4951 0003968 264.7158 95.3548 14.98337281 00
| Epoch (UTC): | 25 May 2026 15:01:13 |
| Eccentricity: | 0.0003968 |
| inclination: | 70.0003° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 120.4951° |
| argument of perigee: | 264.7158° |
| revolutions per day: | 14.98337281 |
| mean anomaly at epoch: | 95.3548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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