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 59553U 26145.64330016 +.00000000 +00000-0 -76203-5 0 00005
2 59553 42.9985 268.9076 0001311 260.7741 99.2963 15.27583113 01
| Epoch (UTC): | 25 May 2026 15:26:21 |
| Eccentricity: | 0.0001311 |
| inclination: | 42.9985° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 268.9076° |
| argument of perigee: | 260.7741° |
| revolutions per day: | 15.27583113 |
| mean anomaly at epoch: | 99.2963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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