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 43647U 26144.39394024 +.00000000 +00000-0 +00000-0 0 00008
2 43647 54.1126 300.8196 0007676 40.4072 319.6276 1.86232305 09
| Epoch (UTC): | 24 May 2026 09:27:16 |
| Eccentricity: | 0.0007676 |
| inclination: | 54.1126° |
| perigee height: | 21507 km |
| apogee height: | 21549 km |
| right ascension of ascending node: | 300.8196° |
| argument of perigee: | 40.4072° |
| revolutions per day: | 1.86232305 |
| mean anomaly at epoch: | 319.6276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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