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 43681U 26145.03720898 +.00000000 +00000-0 +21249-3 0 00001
2 43681 98.0737 349.9855 0010348 117.6359 242.5921 15.09904586 01
| Epoch (UTC): | 25 May 2026 00:53:34 |
| Eccentricity: | 0.0010348 |
| inclination: | 98.0737° |
| perigee height: | 529 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 349.9855° |
| argument of perigee: | 117.6359° |
| revolutions per day: | 15.09904586 |
| mean anomaly at epoch: | 242.5921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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