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 65965U 26145.32414272 +.00000000 +00000-0 +31327-3 0 00006
2 65965 51.8996 6.7897 0000785 106.8929 253.2120 14.79940160 09
| Epoch (UTC): | 25 May 2026 07:46:45 |
| Eccentricity: | 0.0000785 |
| inclination: | 51.8996° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 6.7897° |
| argument of perigee: | 106.8929° |
| revolutions per day: | 14.79940160 |
| mean anomaly at epoch: | 253.2120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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