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 60154U 26145.46628701 +.00000000 +00000-0 +80784-5 0 00003
2 60154 53.1617 323.1141 0001069 101.0001 259.1120 15.30191587 05
| Epoch (UTC): | 25 May 2026 11:11:27 |
| Eccentricity: | 0.0001069 |
| inclination: | 53.1617° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 323.1141° |
| argument of perigee: | 101.0001° |
| revolutions per day: | 15.30191587 |
| mean anomaly at epoch: | 259.1120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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