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 32958U 26020.31189101 +.00000000 +00000-0 +96199-4 0 00002
2 32958 98.6744 324.0358 0008437 187.2240 172.8816 14.19528458 08
| Epoch (UTC): | 20 January 2026 07:29:07 |
| Eccentricity: | 0.0008437 |
| inclination: | 98.6744° |
| perigee height: | 821 km |
| apogee height: | 833 km |
| right ascension of ascending node: | 324.0358° |
| argument of perigee: | 187.2240° |
| revolutions per day: | 14.19528458 |
| mean anomaly at epoch: | 172.8816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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