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 06392U 26121.84960447 +.00000000 +00000-0 +51461-4 0 00008
2 06392 81.2385 333.0975 0054144 332.8263 27.0074 14.08111446 04
| Epoch (UTC): | 01 May 2026 20:23:25 |
| Eccentricity: | 0.0054144 |
| inclination: | 81.2385° |
| perigee height: | 827 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 333.0975° |
| argument of perigee: | 332.8263° |
| revolutions per day: | 14.08111446 |
| mean anomaly at epoch: | 27.0074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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