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 51631U 26145.66196334 +.00000000 +00000-0 -17229-2 0 00009
2 51631 87.8857 40.7750 0002452 84.3336 275.8071 13.10374245 04
| Epoch (UTC): | 25 May 2026 15:53:13 |
| Eccentricity: | 0.0002452 |
| inclination: | 87.8857° |
| perigee height: | 1220 km |
| apogee height: | 1224 km |
| right ascension of ascending node: | 40.7750° |
| argument of perigee: | 84.3336° |
| revolutions per day: | 13.10374245 |
| mean anomaly at epoch: | 275.8071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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