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 65149U 26145.44265494 +.00000000 +00000-0 +32221-3 0 00007
2 65149 51.8958 193.6247 0000411 84.9687 275.1322 14.79940174 01
| Epoch (UTC): | 25 May 2026 10:37:25 |
| Eccentricity: | 0.0000411 |
| inclination: | 51.8958° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 193.6247° |
| argument of perigee: | 84.9687° |
| revolutions per day: | 14.79940174 |
| mean anomaly at epoch: | 275.1322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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