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 32792U 26072.94057523 +.00000000 +00000-0 +17188-3 0 00006
2 32792 98.1448 72.3972 0023027 285.1565 74.7103 14.86115536 07
| Epoch (UTC): | 13 March 2026 22:34:25 |
| Eccentricity: | 0.0023027 |
| inclination: | 98.1448° |
| perigee height: | 594 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 72.3972° |
| argument of perigee: | 285.1565° |
| revolutions per day: | 14.86115536 |
| mean anomaly at epoch: | 74.7103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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