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 57777U 26145.63706124 +.00000000 +00000-0 +47874-4 0 00007
2 57777 43.0011 123.4229 0001149 266.5136 93.5584 15.27579463 04
| Epoch (UTC): | 25 May 2026 15:17:22 |
| Eccentricity: | 0.0001149 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 123.4229° |
| argument of perigee: | 266.5136° |
| revolutions per day: | 15.27579463 |
| mean anomaly at epoch: | 93.5584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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