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 37154U 26103.49790747 +.00000000 +00000-0 +29369-3 0 00004
2 37154 82.4554 102.7486 0015985 89.2419 27.4098 12.43745400 09
| Epoch (UTC): | 13 April 2026 11:56:59 |
| Eccentricity: | 0.0015985 |
| inclination: | 82.4554° |
| perigee height: | 1478 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 102.7486° |
| argument of perigee: | 89.2419° |
| revolutions per day: | 12.43745400 |
| mean anomaly at epoch: | 27.4098° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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