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 43181U 26145.57447332 +.00000000 +00000-0 +94736-4 0 00006
2 43181 97.3608 51.7091 0002033 82.3965 277.7503 15.22846429 00
| Epoch (UTC): | 25 May 2026 13:47:14 |
| Eccentricity: | 0.0002033 |
| inclination: | 97.3608° |
| perigee height: | 496 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 51.7091° |
| argument of perigee: | 82.3965° |
| revolutions per day: | 15.22846429 |
| mean anomaly at epoch: | 277.7503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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