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 65847U 26145.54365198 +.00000000 +00000-0 +61074-3 0 00003
2 65847 53.1576 91.8193 0001101 96.6912 263.4214 15.30219530 07
| Epoch (UTC): | 25 May 2026 13:02:51 |
| Eccentricity: | 0.0001101 |
| inclination: | 53.1576° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 91.8193° |
| argument of perigee: | 96.6912° |
| revolutions per day: | 15.30219530 |
| mean anomaly at epoch: | 263.4214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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