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 61587U 26145.48140038 +.00000000 +00000-0 +65781-3 0 00006
2 61587 53.1589 67.4240 0001122 80.6543 279.4586 15.34404475 03
| Epoch (UTC): | 25 May 2026 11:33:12 |
| Eccentricity: | 0.0001122 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 67.4240° |
| argument of perigee: | 80.6543° |
| revolutions per day: | 15.34404475 |
| mean anomaly at epoch: | 279.4586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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