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 51655U 26145.13774992 +.00000000 +00000-0 +15432-3 0 00003
2 51655 87.9153 10.4565 0002153 68.3097 291.8263 13.17648992 03
| Epoch (UTC): | 25 May 2026 03:18:21 |
| Eccentricity: | 0.0002153 |
| inclination: | 87.9153° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4565° |
| argument of perigee: | 68.3097° |
| revolutions per day: | 13.17648992 |
| mean anomaly at epoch: | 291.8263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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