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 43188U 26106.69557470 +.00000000 +00000-0 +16137-3 0 00006
2 43188 97.5425 12.0663 0007554 218.9359 141.1331 15.16100279 00
| Epoch (UTC): | 16 April 2026 16:41:37 |
| Eccentricity: | 0.0007554 |
| inclination: | 97.5425° |
| perigee height: | 512 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 12.0663° |
| argument of perigee: | 218.9359° |
| revolutions per day: | 15.16100279 |
| mean anomaly at epoch: | 141.1331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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