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 60546U 26145.46015888 +.00000000 +00000-0 +19977-3 0 00008
2 60546 97.6786 222.7949 0003195 167.8371 192.2930 14.99732077 07
| Epoch (UTC): | 25 May 2026 11:02:37 |
| Eccentricity: | 0.0003195 |
| inclination: | 97.6786° |
| perigee height: | 566 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 222.7949° |
| argument of perigee: | 167.8371° |
| revolutions per day: | 14.99732077 |
| mean anomaly at epoch: | 192.2930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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