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 65500U 26144.88209612 +.00000000 +00000-0 +45420-3 0 00000
2 65500 53.1603 277.2190 0001029 90.9393 269.1725 15.30213018 05
| Epoch (UTC): | 24 May 2026 21:10:13 |
| Eccentricity: | 0.0001029 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 277.2190° |
| argument of perigee: | 90.9393° |
| revolutions per day: | 15.30213018 |
| mean anomaly at epoch: | 269.1725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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