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 65867U 26145.41143505 +.00000000 +00000-0 +83933-3 0 00005
2 65867 53.1595 297.6967 0002001 85.7971 274.3258 15.30225881 04
| Epoch (UTC): | 25 May 2026 09:52:27 |
| Eccentricity: | 0.0002001 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 297.6967° |
| argument of perigee: | 85.7971° |
| revolutions per day: | 15.30225881 |
| mean anomaly at epoch: | 274.3258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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