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 18748U 26097.87501840 +.00000000 +00000-0 +17622-3 0 00009
2 18748 82.4194 68.2016 0007995 232.3372 127.7207 16.48562782 08
| Epoch (UTC): | 07 April 2026 21:00:01 |
| Eccentricity: | 0.0007995 |
| inclination: | 82.4194° |
| perigee height: | 138 km |
| apogee height: | 148 km |
| right ascension of ascending node: | 68.2016° |
| argument of perigee: | 232.3372° |
| revolutions per day: | 16.48562782 |
| mean anomaly at epoch: | 127.7207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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