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 43789U 26046.91687850 +.00000000 +00000-0 +80964-3 0 00006
2 43789 97.4099 130.1753 0010600 276.9538 83.0556 16.40712868 08
| Epoch (UTC): | 15 February 2026 22:00:18 |
| Eccentricity: | 0.0010600 |
| inclination: | 97.4099° |
| perigee height: | 157 km |
| apogee height: | 171 km |
| right ascension of ascending node: | 130.1753° |
| argument of perigee: | 276.9538° |
| revolutions per day: | 16.40712868 |
| mean anomaly at epoch: | 83.0556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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