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 57633U 26145.05535698 +.00000000 +00000-0 +71177-5 0 00004
2 57633 43.0038 21.4420 0001058 203.8170 156.2633 15.27574056 00
| Epoch (UTC): | 25 May 2026 01:19:42 |
| Eccentricity: | 0.0001058 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.4420° |
| argument of perigee: | 203.8170° |
| revolutions per day: | 15.27574056 |
| mean anomaly at epoch: | 156.2633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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