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 26131.31200734 +.00000000 +00000-0 +13885-3 0 00008
2 43188 97.5404 36.5253 0010054 134.1742 226.0319 15.16326659 08
| Epoch (UTC): | 11 May 2026 07:29:17 |
| Eccentricity: | 0.0010054 |
| inclination: | 97.5404° |
| perigee height: | 510 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 36.5253° |
| argument of perigee: | 134.1742° |
| revolutions per day: | 15.16326659 |
| mean anomaly at epoch: | 226.0319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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