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 59019U 26145.53841139 +.00000000 +00000-0 +51711-4 0 00008
2 59019 53.1608 81.5538 0001300 99.4544 260.6603 15.30193815 07
| Epoch (UTC): | 25 May 2026 12:55:18 |
| Eccentricity: | 0.0001300 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.5538° |
| argument of perigee: | 99.4544° |
| revolutions per day: | 15.30193815 |
| mean anomaly at epoch: | 260.6603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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