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 18153U 26076.15409148 +.00000000 +00000-0 +50484-4 0 00009
2 18153 82.5028 341.9983 0020460 353.5199 6.5749 14.85637798 08
| Epoch (UTC): | 17 March 2026 03:41:53 |
| Eccentricity: | 0.0020460 |
| inclination: | 82.5028° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 341.9983° |
| argument of perigee: | 353.5199° |
| revolutions per day: | 14.85637798 |
| mean anomaly at epoch: | 6.5749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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