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 65392U 26145.37706431 +.00000000 +00000-0 +25781-3 0 00003
2 65392 97.4507 16.8125 0002270 82.3810 277.7675 15.05658283 09
| Epoch (UTC): | 25 May 2026 09:02:58 |
| Eccentricity: | 0.0002270 |
| inclination: | 97.4507° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.8125° |
| argument of perigee: | 82.3810° |
| revolutions per day: | 15.05658283 |
| mean anomaly at epoch: | 277.7675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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