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 55154U 26145.11864019 +.00000000 +00000-0 +15420-2 0 00005
2 55154 87.8908 25.6590 0001068 84.2027 275.9222 13.11416017 01
| Epoch (UTC): | 25 May 2026 02:50:50 |
| Eccentricity: | 0.0001068 |
| inclination: | 87.8908° |
| perigee height: | 1217 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 25.6590° |
| argument of perigee: | 84.2027° |
| revolutions per day: | 13.11416017 |
| mean anomaly at epoch: | 275.9222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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