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 57877U 26145.55117310 +.00000000 +00000-0 +19671-4 0 00006
2 57877 43.0005 174.4862 0001489 275.3002 84.7679 15.27587393 02
| Epoch (UTC): | 25 May 2026 13:13:41 |
| Eccentricity: | 0.0001489 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.4862° |
| argument of perigee: | 275.3002° |
| revolutions per day: | 15.27587393 |
| mean anomaly at epoch: | 84.7679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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