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 59133U 26145.35102286 +.00000000 +00000-0 +30744-3 0 00000
2 59133 97.5575 289.4488 0006846 299.6508 60.4057 15.42676422 08
| Epoch (UTC): | 25 May 2026 08:25:28 |
| Eccentricity: | 0.0006846 |
| inclination: | 97.5575° |
| perigee height: | 434 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 289.4488° |
| argument of perigee: | 299.6508° |
| revolutions per day: | 15.42676422 |
| mean anomaly at epoch: | 60.4057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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