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 18152U 26021.46333145 +.00000000 +00000-0 +47670-3 0 00007
2 18152 82.4862 95.2190 0009642 173.6203 186.5162 15.29667471 05
| Epoch (UTC): | 21 January 2026 11:07:11 |
| Eccentricity: | 0.0009642 |
| inclination: | 82.4862° |
| perigee height: | 470 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 95.2190° |
| argument of perigee: | 173.6203° |
| revolutions per day: | 15.29667471 |
| mean anomaly at epoch: | 186.5162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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