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 59127U 26145.39070159 +.00000000 +00000-0 +34847-3 0 00008
2 59127 97.5552 289.4963 0005707 302.7994 57.2703 15.43746445 00
| Epoch (UTC): | 25 May 2026 09:22:36 |
| Eccentricity: | 0.0005707 |
| inclination: | 97.5552° |
| perigee height: | 431 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 289.4963° |
| argument of perigee: | 302.7994° |
| revolutions per day: | 15.43746445 |
| mean anomaly at epoch: | 57.2703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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