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 18361U 26087.93415184 +.00000000 +00000-0 +14298-3 0 00007
2 18361 90.3652 83.1833 0101843 280.6882 78.2811 13.44927610 07
| Epoch (UTC): | 28 March 2026 22:25:10 |
| Eccentricity: | 0.0101843 |
| inclination: | 90.3652° |
| perigee height: | 1015 km |
| apogee height: | 1167 km |
| right ascension of ascending node: | 83.1833° |
| argument of perigee: | 280.6882° |
| revolutions per day: | 13.44927610 |
| mean anomaly at epoch: | 78.2811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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