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 43113U 26145.34428595 +.00000000 +00000-0 +13084-3 0 00002
2 43113 99.2446 60.6558 0351164 149.4521 212.7658 14.67665784 09
| Epoch (UTC): | 25 May 2026 08:15:46 |
| Eccentricity: | 0.0351164 |
| inclination: | 99.2446° |
| perigee height: | 421 km |
| apogee height: | 916 km |
| right ascension of ascending node: | 60.6558° |
| argument of perigee: | 149.4521° |
| revolutions per day: | 14.67665784 |
| mean anomaly at epoch: | 212.7658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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