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 62892U 26145.57894161 +.00000000 +00000-0 +47781-3 0 00009
2 62892 43.0008 251.2677 0000819 256.7963 103.2797 15.27567667 01
| Epoch (UTC): | 25 May 2026 13:53:40 |
| Eccentricity: | 0.0000819 |
| inclination: | 43.0008° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.2677° |
| argument of perigee: | 256.7963° |
| revolutions per day: | 15.27567667 |
| mean anomaly at epoch: | 103.2797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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