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 65389U 26145.62627346 +.00000000 +00000-0 +21167-3 0 00008
2 65389 97.4480 16.9331 0002358 82.1558 277.9937 15.05658892 08
| Epoch (UTC): | 25 May 2026 15:01:50 |
| Eccentricity: | 0.0002358 |
| inclination: | 97.4480° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.9331° |
| argument of perigee: | 82.1558° |
| revolutions per day: | 15.05658892 |
| mean anomaly at epoch: | 277.9937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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