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 51656U 26145.60884272 +.00000000 +00000-0 +11936-3 0 00004
2 51656 97.5120 152.6035 0001745 90.2909 269.8522 15.12724457 09
| Epoch (UTC): | 25 May 2026 14:36:44 |
| Eccentricity: | 0.0001745 |
| inclination: | 97.5120° |
| perigee height: | 527 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 152.6035° |
| argument of perigee: | 90.2909° |
| revolutions per day: | 15.12724457 |
| mean anomaly at epoch: | 269.8522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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