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 26073.57102420 +.00000000 +00000-0 +99484-4 0 00004
2 18096 74.0401 119.3026 0022417 228.9659 130.9558 14.37958880 05
| Epoch (UTC): | 14 March 2026 13:42:16 |
| Eccentricity: | 0.0022417 |
| inclination: | 74.0401° |
| perigee height: | 749 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 119.3026° |
| argument of perigee: | 228.9659° |
| revolutions per day: | 14.37958880 |
| mean anomaly at epoch: | 130.9558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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