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 43717U 26145.61904714 +.00000000 +00000-0 +98297-4 0 00004
2 43717 97.9556 218.2541 0001150 83.5518 276.5823 14.77082312 03
| Epoch (UTC): | 25 May 2026 14:51:25 |
| Eccentricity: | 0.0001150 |
| inclination: | 97.9556° |
| perigee height: | 638 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 218.2541° |
| argument of perigee: | 83.5518° |
| revolutions per day: | 14.77082312 |
| mean anomaly at epoch: | 276.5823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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