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 51148U 26145.50504397 +.00000000 +00000-0 +15645-2 0 00006
2 51148 53.2176 323.4630 0001868 97.9531 262.1675 15.12233810 08
| Epoch (UTC): | 25 May 2026 12:07:15 |
| Eccentricity: | 0.0001868 |
| inclination: | 53.2176° |
| perigee height: | 528 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 323.4630° |
| argument of perigee: | 97.9531° |
| revolutions per day: | 15.12233810 |
| mean anomaly at epoch: | 262.1675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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