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 65019U 26144.75623249 +.00000000 +00000-0 +57123-3 0 00000
2 65019 53.1616 301.0494 0001170 79.2276 280.8856 15.30210622 07
| Epoch (UTC): | 24 May 2026 18:08:58 |
| Eccentricity: | 0.0001170 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 301.0494° |
| argument of perigee: | 79.2276° |
| revolutions per day: | 15.30210622 |
| mean anomaly at epoch: | 280.8856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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