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 65994U 26145.52082728 +.00000000 +00000-0 +96605-4 0 00008
2 65994 81.3018 233.1964 0000944 125.8312 234.2930 13.79430682 09
| Epoch (UTC): | 25 May 2026 12:29:59 |
| Eccentricity: | 0.0000944 |
| inclination: | 81.3018° |
| perigee height: | 965 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 233.1964° |
| argument of perigee: | 125.8312° |
| revolutions per day: | 13.79430682 |
| mean anomaly at epoch: | 234.2930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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