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 18187U 26041.33494348 +.00000000 +00000-0 +30035-4 0 00004
2 18187 65.0113 23.3084 0014120 276.6645 83.2833 14.31498574 00
| Epoch (UTC): | 10 February 2026 08:02:19 |
| Eccentricity: | 0.0014120 |
| inclination: | 65.0113° |
| perigee height: | 777 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 23.3084° |
| argument of perigee: | 276.6645° |
| revolutions per day: | 14.31498574 |
| mean anomaly at epoch: | 83.2833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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