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 43792U 26111.83415058 +.00000000 +00000-0 +77201-4 0 00004
2 43792 97.4037 151.6267 0012862 157.1638 203.0163 15.04073432 09
| Epoch (UTC): | 21 April 2026 20:01:10 |
| Eccentricity: | 0.0012862 |
| inclination: | 97.4037° |
| perigee height: | 545 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 151.6267° |
| argument of perigee: | 157.1638° |
| revolutions per day: | 15.04073432 |
| mean anomaly at epoch: | 203.0163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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