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 65512U 26145.64731176 +.00000000 +00000-0 +48875-3 0 00000
2 65512 53.1581 272.7544 0000871 71.0670 289.0427 15.34394938 03
| Epoch (UTC): | 25 May 2026 15:32:07 |
| Eccentricity: | 0.0000871 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 272.7544° |
| argument of perigee: | 71.0670° |
| revolutions per day: | 15.34394938 |
| mean anomaly at epoch: | 289.0427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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