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 43672U 26145.03565691 +.00000000 +00000-0 +17304-3 0 00006
2 43672 97.8775 256.8192 0001390 93.6717 266.4656 14.84238039 03
| Epoch (UTC): | 25 May 2026 00:51:20 |
| Eccentricity: | 0.0001390 |
| inclination: | 97.8775° |
| perigee height: | 615 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 256.8192° |
| argument of perigee: | 93.6717° |
| revolutions per day: | 14.84238039 |
| mean anomaly at epoch: | 266.4656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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