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 26088.18092279 +.00000000 +00000-0 +12839-3 0 00005
2 18096 74.0390 92.4019 0021900 199.4252 160.6070 14.37968159 01
| Epoch (UTC): | 29 March 2026 04:20:31 |
| Eccentricity: | 0.0021900 |
| inclination: | 74.0390° |
| perigee height: | 750 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 92.4019° |
| argument of perigee: | 199.4252° |
| revolutions per day: | 14.37968159 |
| mean anomaly at epoch: | 160.6070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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