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 56332U 26145.44688308 +.00000000 +00000-0 +23678-4 0 00001
2 56332 97.4449 145.3921 0001874 87.4025 272.7417 15.05647419 01
| Epoch (UTC): | 25 May 2026 10:43:30 |
| Eccentricity: | 0.0001874 |
| inclination: | 97.4449° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.3921° |
| argument of perigee: | 87.4025° |
| revolutions per day: | 15.05647419 |
| mean anomaly at epoch: | 272.7417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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