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 29092U 26071.64652471 +.00000000 +00000-0 +13296-3 0 00000
2 29092 97.7552 94.8142 0001495 94.5751 265.5637 14.87592543 09
| Epoch (UTC): | 12 March 2026 15:30:59 |
| Eccentricity: | 0.0001495 |
| inclination: | 97.7552° |
| perigee height: | 604 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 94.8142° |
| argument of perigee: | 94.5751° |
| revolutions per day: | 14.87592543 |
| mean anomaly at epoch: | 265.5637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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