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 26104.34325477 +.00000000 +00000-0 +21329-3 0 00005
2 00932 81.3379 67.6261 1119786 53.1853 316.6782 12.67150196 04
| Epoch (UTC): | 14 April 2026 08:14:17 |
| Eccentricity: | 0.1119786 |
| inclination: | 81.3379° |
| perigee height: | 523 km |
| apogee height: | 2264 km |
| right ascension of ascending node: | 67.6261° |
| argument of perigee: | 53.1853° |
| revolutions per day: | 12.67150196 |
| mean anomaly at epoch: | 316.6782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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