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 65396U 26145.36874838 +.00000000 +00000-0 +33009-3 0 00005
2 65396 97.4484 16.6667 0003090 86.5252 273.6328 15.05657009 08
| Epoch (UTC): | 25 May 2026 08:50:59 |
| Eccentricity: | 0.0003090 |
| inclination: | 97.4484° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 16.6667° |
| argument of perigee: | 86.5252° |
| revolutions per day: | 15.05657009 |
| mean anomaly at epoch: | 273.6328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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