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 26139.87826294 +.00000000 +00000-0 +00000-0 0 00001
2 23132 12.3554 5.8850 0002452 313.7023 224.6756 1.00268795 01
| Epoch (UTC): | 19 May 2026 21:04:41 |
| Eccentricity: | 0.0002452 |
| inclination: | 12.3554° |
| perigee height: | 35777 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 5.8850° |
| argument of perigee: | 313.7023° |
| revolutions per day: | 1.00268795 |
| mean anomaly at epoch: | 224.6756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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