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 65851U 26145.73895781 +.00000000 +00000-0 +17759-3 0 00006
2 65851 34.9895 36.5188 0003145 276.0129 84.0217 14.91753759 09
| Epoch (UTC): | 25 May 2026 17:44:05 |
| Eccentricity: | 0.0003145 |
| inclination: | 34.9895° |
| perigee height: | 590 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 36.5188° |
| argument of perigee: | 276.0129° |
| revolutions per day: | 14.91753759 |
| mean anomaly at epoch: | 84.0217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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