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 57884U 26145.21073332 +.00000000 +00000-0 +37961-4 0 00004
2 57884 43.0020 212.7549 0001311 274.5834 85.4868 15.27571380 00
| Epoch (UTC): | 25 May 2026 05:03:27 |
| Eccentricity: | 0.0001311 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 212.7549° |
| argument of perigee: | 274.5834° |
| revolutions per day: | 15.27571380 |
| mean anomaly at epoch: | 85.4868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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