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 43175U 26144.93261743 +.00000000 +00000-0 +00000-0 0 00005
2 43175 0.0274 38.1976 0000990 16.2794 116.2932 1.00271473 05
| Epoch (UTC): | 24 May 2026 22:22:58 |
| Eccentricity: | 0.0000990 |
| inclination: | 0.0274° |
| perigee height: | 35783 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 38.1976° |
| argument of perigee: | 16.2794° |
| revolutions per day: | 1.00271473 |
| mean anomaly at epoch: | 116.2932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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