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 04159U 26018.48308503 +.00000000 +00000-0 +67179-4 0 00004
2 04159 69.9612 176.2248 0113484 146.7885 214.0399 13.72882433 03
| Epoch (UTC): | 18 January 2026 11:35:38 |
| Eccentricity: | 0.0113484 |
| inclination: | 69.9612° |
| perigee height: | 906 km |
| apogee height: | 1073 km |
| right ascension of ascending node: | 176.2248° |
| argument of perigee: | 146.7885° |
| revolutions per day: | 13.72882433 |
| mean anomaly at epoch: | 214.0399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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