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 43613U 26152.17811014 +.00000000 +00000-0 +40534-3 0 00008
2 43613 92.0067 286.6559 0004121 120.9396 239.2258 15.28340118 06
| Epoch (UTC): | 01 June 2026 04:16:28 |
| Eccentricity: | 0.0004121 |
| inclination: | 92.0067° |
| perigee height: | 478 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 286.6559° |
| argument of perigee: | 120.9396° |
| revolutions per day: | 15.28340118 |
| mean anomaly at epoch: | 239.2258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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