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 60574U 26145.50124450 +.00000000 +00000-0 +34806-3 0 00008
2 60574 97.7015 223.7670 0006785 193.7191 166.3850 15.00972224 08
| Epoch (UTC): | 25 May 2026 12:01:47 |
| Eccentricity: | 0.0006785 |
| inclination: | 97.7015° |
| perigee height: | 559 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 223.7670° |
| argument of perigee: | 193.7191° |
| revolutions per day: | 15.00972224 |
| mean anomaly at epoch: | 166.3850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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