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 43189U 26106.97420552 +.00000000 +00000-0 +15796-3 0 00008
2 43189 97.5442 12.4086 0009151 210.8721 149.1975 15.16058130 02
| Epoch (UTC): | 16 April 2026 23:22:51 |
| Eccentricity: | 0.0009151 |
| inclination: | 97.5442° |
| perigee height: | 511 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 12.4086° |
| argument of perigee: | 210.8721° |
| revolutions per day: | 15.16058130 |
| mean anomaly at epoch: | 149.1975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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