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 60920U 26145.38729561 +.00000000 +00000-0 +24565-4 0 00005
2 60920 53.1617 287.8765 0001218 97.0883 263.0256 15.30192749 07
| Epoch (UTC): | 25 May 2026 09:17:42 |
| Eccentricity: | 0.0001218 |
| inclination: | 53.1617° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.8765° |
| argument of perigee: | 97.0883° |
| revolutions per day: | 15.30192749 |
| mean anomaly at epoch: | 263.0256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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