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 65665U 26145.58134792 +.00000000 +00000-0 +17357-3 0 00004
2 65665 97.4473 189.5082 0002067 104.4410 255.7047 15.05655205 00
| Epoch (UTC): | 25 May 2026 13:57:08 |
| Eccentricity: | 0.0002067 |
| inclination: | 97.4473° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.5082° |
| argument of perigee: | 104.4410° |
| revolutions per day: | 15.05655205 |
| mean anomaly at epoch: | 255.7047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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