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 68556U 26145.63484544 +.00000000 +00000-0 +91015-3 0 00008
2 68556 53.1600 4.5873 0001174 94.0776 266.0361 15.34411186 08
| Epoch (UTC): | 25 May 2026 15:14:10 |
| Eccentricity: | 0.0001174 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 4.5873° |
| argument of perigee: | 94.0776° |
| revolutions per day: | 15.34411186 |
| mean anomaly at epoch: | 266.0361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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