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 24932U 26032.33876700 +.00000000 +00000-0 +00000-0 0 00000
2 24932 13.5818 15.9028 0006538 34.3949 157.0186 0.98310020 08
| Epoch (UTC): | 01 February 2026 08:07:49 |
| Eccentricity: | 0.0006538 |
| inclination: | 13.5818° |
| perigee height: | 36318 km |
| apogee height: | 36374 km |
| right ascension of ascending node: | 15.9028° |
| argument of perigee: | 34.3949° |
| revolutions per day: | 0.98310020 |
| mean anomaly at epoch: | 157.0186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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