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 64040U 26145.42759638 +.00000000 +00000-0 +20305-3 0 00002
2 64040 70.0008 281.0891 0002592 269.9414 90.1448 14.98334795 02
| Epoch (UTC): | 25 May 2026 10:15:44 |
| Eccentricity: | 0.0002592 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.0891° |
| argument of perigee: | 269.9414° |
| revolutions per day: | 14.98334795 |
| mean anomaly at epoch: | 90.1448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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