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 54151U 26145.61624618 +.00000000 +00000-0 +97161-4 0 00009
2 54151 82.4998 1.3988 0015804 282.8654 77.0660 12.42890346 05
| Epoch (UTC): | 25 May 2026 14:47:23 |
| Eccentricity: | 0.0015804 |
| inclination: | 82.4998° |
| perigee height: | 1482 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 1.3988° |
| argument of perigee: | 282.8654° |
| revolutions per day: | 12.42890346 |
| mean anomaly at epoch: | 77.0660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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