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 65437U 26145.33987528 +.00000000 +00000-0 +27358-3 0 00009
2 65437 97.4487 359.5960 0001904 77.9519 282.1922 15.05655971 05
| Epoch (UTC): | 25 May 2026 08:09:25 |
| Eccentricity: | 0.0001904 |
| inclination: | 97.4487° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.5960° |
| argument of perigee: | 77.9519° |
| revolutions per day: | 15.05655971 |
| mean anomaly at epoch: | 282.1922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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