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 23753U 26088.16641536 +.00000000 +00000-0 +47653-4 0 00008
2 23753 98.7109 159.1681 0003066 340.4229 19.6833 14.27017281 09
| Epoch (UTC): | 29 March 2026 03:59:38 |
| Eccentricity: | 0.0003066 |
| inclination: | 98.7109° |
| perigee height: | 800 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 159.1681° |
| argument of perigee: | 340.4229° |
| revolutions per day: | 14.27017281 |
| mean anomaly at epoch: | 19.6833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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