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 57184U 26145.58284225 +.00000000 +00000-0 +23120-3 0 00003
2 57184 97.5088 204.0141 0011240 183.0906 177.0261 15.18661812 04
| Epoch (UTC): | 25 May 2026 13:59:17 |
| Eccentricity: | 0.0011240 |
| inclination: | 97.5088° |
| perigee height: | 502 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 204.0141° |
| argument of perigee: | 183.0906° |
| revolutions per day: | 15.18661812 |
| mean anomaly at epoch: | 177.0261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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