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 65675U 26145.55920209 +.00000000 +00000-0 +33864-3 0 00009
2 65675 97.4462 189.5406 0002594 124.7395 235.4076 15.05665308 03
| Epoch (UTC): | 25 May 2026 13:25:15 |
| Eccentricity: | 0.0002594 |
| inclination: | 97.4462° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.5406° |
| argument of perigee: | 124.7395° |
| revolutions per day: | 15.05665308 |
| mean anomaly at epoch: | 235.4076° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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