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 00932U 26088.07873293 +.00000000 +00000-0 +22135-3 0 00006
2 00932 81.3353 80.1427 1119776 90.0399 282.8755 12.67124281 04
| Epoch (UTC): | 29 March 2026 01:53:22 |
| Eccentricity: | 0.1119776 |
| inclination: | 81.3353° |
| perigee height: | 523 km |
| apogee height: | 2264 km |
| right ascension of ascending node: | 80.1427° |
| argument of perigee: | 90.0399° |
| revolutions per day: | 12.67124281 |
| mean anomaly at epoch: | 282.8755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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