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 65456U 26145.32603551 +.00000000 +00000-0 +46190-3 0 00005
2 65456 97.4496 359.6163 0002260 94.0821 266.0665 15.05654869 04
| Epoch (UTC): | 25 May 2026 07:49:29 |
| Eccentricity: | 0.0002260 |
| inclination: | 97.4496° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.6163° |
| argument of perigee: | 94.0821° |
| revolutions per day: | 15.05654869 |
| mean anomaly at epoch: | 266.0665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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