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 25359U 26064.58688280 +.00000000 +00000-0 -56609-4 0 00001
2 25359 26.3884 15.8237 0513348 228.3863 298.9296 12.94614197 08
| Epoch (UTC): | 05 March 2026 14:05:06 |
| Eccentricity: | 0.0513348 |
| inclination: | 26.3884° |
| perigee height: | 890 km |
| apogee height: | 1677 km |
| right ascension of ascending node: | 15.8237° |
| argument of perigee: | 228.3863° |
| revolutions per day: | 12.94614197 |
| mean anomaly at epoch: | 298.9296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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