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 26044.33899928 +.00000000 +00000-0 +38012-4 0 00003
2 18187 65.0118 14.8958 0014161 276.9731 82.9743 14.31499117 04
| Epoch (UTC): | 13 February 2026 08:08:09 |
| Eccentricity: | 0.0014161 |
| inclination: | 65.0118° |
| perigee height: | 777 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 14.8958° |
| argument of perigee: | 276.9731° |
| revolutions per day: | 14.31499117 |
| mean anomaly at epoch: | 82.9743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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