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 65144U 26145.46592598 +.00000000 +00000-0 +32297-3 0 00005
2 65144 51.8919 166.0308 0008319 0.4205 359.6770 14.96890654 00
| Epoch (UTC): | 25 May 2026 11:10:56 |
| Eccentricity: | 0.0008319 |
| inclination: | 51.8919° |
| perigee height: | 571 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 166.0308° |
| argument of perigee: | 0.4205° |
| revolutions per day: | 14.96890654 |
| mean anomaly at epoch: | 359.6770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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