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 59273U 26145.39959023 +.00000000 +00000-0 +30411-4 0 00000
2 59273 53.1595 184.6671 0001003 82.7354 277.3761 15.30198126 01
| Epoch (UTC): | 25 May 2026 09:35:24 |
| Eccentricity: | 0.0001003 |
| inclination: | 53.1595° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.6671° |
| argument of perigee: | 82.7354° |
| revolutions per day: | 15.30198126 |
| mean anomaly at epoch: | 277.3761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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