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 23712U 26140.39146352 +.00000000 +00000-0 +00000-0 0 00004
2 23712 14.0638 3.9595 0000496 92.8383 178.5680 1.00366611 01
| Epoch (UTC): | 20 May 2026 09:23:42 |
| Eccentricity: | 0.0000496 |
| inclination: | 14.0638° |
| perigee height: | 35758 km |
| apogee height: | 35762 km |
| right ascension of ascending node: | 3.9595° |
| argument of perigee: | 92.8383° |
| revolutions per day: | 1.00366611 |
| mean anomaly at epoch: | 178.5680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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