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 56154U 26145.35749616 +.00000000 +00000-0 +88287-4 0 00000
2 56154 97.4988 332.8293 0001594 97.3221 262.8192 15.14304200 01
| Epoch (UTC): | 25 May 2026 08:34:47 |
| Eccentricity: | 0.0001594 |
| inclination: | 97.4988° |
| perigee height: | 522 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 332.8293° |
| argument of perigee: | 97.3221° |
| revolutions per day: | 15.14304200 |
| mean anomaly at epoch: | 262.8192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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