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 43286U 26144.88171424 +.00000000 +00000-0 +00000-0 0 00008
2 43286 29.1250 74.5548 0017489 178.6700 1.6558 1.00273959 06
| Epoch (UTC): | 24 May 2026 21:09:40 |
| Eccentricity: | 0.0017489 |
| inclination: | 29.1250° |
| perigee height: | 35712 km |
| apogee height: | 35860 km |
| right ascension of ascending node: | 74.5548° |
| argument of perigee: | 178.6700° |
| revolutions per day: | 1.00273959 |
| mean anomaly at epoch: | 1.6558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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