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 43335U 26088.22307176 +.00000000 +00000-0 +13091-2 0 00009
2 43335 82.9415 181.9444 0044169 86.1903 274.4307 13.85812180 05
| Epoch (UTC): | 29 March 2026 05:21:13 |
| Eccentricity: | 0.0044169 |
| inclination: | 82.9415° |
| perigee height: | 911 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 181.9444° |
| argument of perigee: | 86.1903° |
| revolutions per day: | 13.85812180 |
| mean anomaly at epoch: | 274.4307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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