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 55174U 26145.05761441 +.00000000 +00000-0 +73328-3 0 00007
2 55174 87.8908 25.6685 0002351 95.9876 264.1519 13.11415216 04
| Epoch (UTC): | 25 May 2026 01:22:57 |
| Eccentricity: | 0.0002351 |
| inclination: | 87.8908° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6685° |
| argument of perigee: | 95.9876° |
| revolutions per day: | 13.11415216 |
| mean anomaly at epoch: | 264.1519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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