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 59775U 26145.57454806 +.00000000 +00000-0 +35197-3 0 00001
2 59775 97.6601 275.8594 0007707 260.6539 99.3829 15.28916730 08
| Epoch (UTC): | 25 May 2026 13:47:20 |
| Eccentricity: | 0.0007707 |
| inclination: | 97.6601° |
| perigee height: | 474 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 275.8594° |
| argument of perigee: | 260.6539° |
| revolutions per day: | 15.28916730 |
| mean anomaly at epoch: | 99.3829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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