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 65398U 26145.23029993 +.00000000 +00000-0 +93328-3 0 00007
2 65398 97.4483 16.5463 0002441 89.7695 270.3812 15.05653317 07
| Epoch (UTC): | 25 May 2026 05:31:37 |
| Eccentricity: | 0.0002441 |
| inclination: | 97.4483° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.5463° |
| argument of perigee: | 89.7695° |
| revolutions per day: | 15.05653317 |
| mean anomaly at epoch: | 270.3812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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