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 26018.65036679 +.00000000 +00000-0 +23116-3 0 00005
2 18152 82.4870 98.0620 0009419 183.3966 176.7211 15.29584071 09
| Epoch (UTC): | 18 January 2026 15:36:31 |
| Eccentricity: | 0.0009419 |
| inclination: | 82.4870° |
| perigee height: | 471 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 98.0620° |
| argument of perigee: | 183.3966° |
| revolutions per day: | 15.29584071 |
| mean anomaly at epoch: | 176.7211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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