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 61590U 26145.51296169 +.00000000 +00000-0 +22835-4 0 00005
2 61590 53.1620 67.6239 0001269 78.3161 281.7984 15.34385194 09
| Epoch (UTC): | 25 May 2026 12:18:39 |
| Eccentricity: | 0.0001269 |
| inclination: | 53.1620° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 67.6239° |
| argument of perigee: | 78.3161° |
| revolutions per day: | 15.34385194 |
| mean anomaly at epoch: | 281.7984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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