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 53670U 26145.24332616 +.00000000 +00000-0 -83884-4 0 00005
2 53670 97.4506 26.3324 0002276 72.9173 287.2303 15.05650029 08
| Epoch (UTC): | 25 May 2026 05:50:23 |
| Eccentricity: | 0.0002276 |
| inclination: | 97.4506° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 26.3324° |
| argument of perigee: | 72.9173° |
| revolutions per day: | 15.05650029 |
| mean anomaly at epoch: | 287.2303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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