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 43017U 26075.87985970 +.00000000 +00000-0 +32589-3 0 00001
2 43017 97.4856 305.0257 0153524 287.1888 71.2585 15.11036789 09
| Epoch (UTC): | 16 March 2026 21:06:59 |
| Eccentricity: | 0.0153524 |
| inclination: | 97.4856° |
| perigee height: | 427 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 305.0257° |
| argument of perigee: | 287.1888° |
| revolutions per day: | 15.11036789 |
| mean anomaly at epoch: | 71.2585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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