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 65192U 26145.38672330 +.00000000 +00000-0 +20999-3 0 00008
2 65192 97.4520 17.9135 0002132 77.4296 282.7170 15.05655578 05
| Epoch (UTC): | 25 May 2026 09:16:52 |
| Eccentricity: | 0.0002132 |
| inclination: | 97.4520° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.9135° |
| argument of perigee: | 77.4296° |
| revolutions per day: | 15.05655578 |
| mean anomaly at epoch: | 282.7170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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