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 37190U 26145.48198954 +.00000000 +00000-0 +83318-4 0 00006
2 37190 52.0003 177.2576 0000214 22.6295 124.6024 12.62261803 00
| Epoch (UTC): | 25 May 2026 11:34:03 |
| Eccentricity: | 0.0000214 |
| inclination: | 52.0003° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 177.2576° |
| argument of perigee: | 22.6295° |
| revolutions per day: | 12.62261803 |
| mean anomaly at epoch: | 124.6024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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