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 26072.10516588 +.00000000 +00000-0 +63628-3 0 00007
2 43017 97.4871 301.3303 0154280 300.1874 58.4150 15.10964684 06
| Epoch (UTC): | 13 March 2026 02:31:26 |
| Eccentricity: | 0.0154280 |
| inclination: | 97.4871° |
| perigee height: | 427 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 301.3303° |
| argument of perigee: | 300.1874° |
| revolutions per day: | 15.10964684 |
| mean anomaly at epoch: | 58.4150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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