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 60929U 26145.47973512 +.00000000 +00000-0 +61714-5 0 00009
2 60929 53.1592 322.6650 0000843 99.9887 260.1226 15.69711466 07
| Epoch (UTC): | 25 May 2026 11:30:49 |
| Eccentricity: | 0.0000843 |
| inclination: | 53.1592° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 322.6650° |
| argument of perigee: | 99.9887° |
| revolutions per day: | 15.69711466 |
| mean anomaly at epoch: | 260.1226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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