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 67858U 26145.44882975 +.00000000 +00000-0 +20547-3 0 00003
2 67858 53.1580 205.8923 0001132 79.4576 280.6554 15.34399988 01
| Epoch (UTC): | 25 May 2026 10:46:18 |
| Eccentricity: | 0.0001132 |
| inclination: | 53.1580° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 205.8923° |
| argument of perigee: | 79.4576° |
| revolutions per day: | 15.34399988 |
| mean anomaly at epoch: | 280.6554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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