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 23132U 26145.86705183 +.00000000 +00000-0 +00000-0 0 00000
2 23132 12.3580 5.8483 0002203 310.1398 230.0652 1.00268943 03
| Epoch (UTC): | 25 May 2026 20:48:33 |
| Eccentricity: | 0.0002203 |
| inclination: | 12.3580° |
| perigee height: | 35778 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 5.8483° |
| argument of perigee: | 310.1398° |
| revolutions per day: | 1.00268943 |
| mean anomaly at epoch: | 230.0652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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