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 62760U 26144.95009500 +.00000000 +00000-0 +61655-3 0 00005
2 62760 53.1601 327.7314 0000914 96.7977 263.3129 15.34412644 05
| Epoch (UTC): | 24 May 2026 22:48:08 |
| Eccentricity: | 0.0000914 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 327.7314° |
| argument of perigee: | 96.7977° |
| revolutions per day: | 15.34412644 |
| mean anomaly at epoch: | 263.3129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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