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 18096U 26072.87531281 +.00000000 +00000-0 +93521-4 0 00003
2 18096 74.0402 120.5836 0022438 230.3525 129.5650 14.37958346 05
| Epoch (UTC): | 13 March 2026 21:00:27 |
| Eccentricity: | 0.0022438 |
| inclination: | 74.0402° |
| perigee height: | 749 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 120.5836° |
| argument of perigee: | 230.3525° |
| revolutions per day: | 14.37958346 |
| mean anomaly at epoch: | 129.5650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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