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 65386U 26145.58751273 +.00000000 +00000-0 +15740-3 0 00007
2 65386 97.4515 16.9887 0001980 75.9955 284.1493 15.05657181 08
| Epoch (UTC): | 25 May 2026 14:06:01 |
| Eccentricity: | 0.0001980 |
| inclination: | 97.4515° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.9887° |
| argument of perigee: | 75.9955° |
| revolutions per day: | 15.05657181 |
| mean anomaly at epoch: | 284.1493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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