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 62819U 26145.46739454 +.00000000 +00000-0 +33896-3 0 00001
2 62819 53.1596 312.9535 0001511 97.8371 262.2802 15.30201222 08
| Epoch (UTC): | 25 May 2026 11:13:02 |
| Eccentricity: | 0.0001511 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 312.9535° |
| argument of perigee: | 97.8371° |
| revolutions per day: | 15.30201222 |
| mean anomaly at epoch: | 262.2802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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