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 53072U 26145.47176229 +.00000000 +00000-0 -10186-3 0 00006
2 53072 97.4458 326.4805 0001400 126.3577 233.7780 15.05658561 02
| Epoch (UTC): | 25 May 2026 11:19:20 |
| Eccentricity: | 0.0001400 |
| inclination: | 97.4458° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 326.4805° |
| argument of perigee: | 126.3577° |
| revolutions per day: | 15.05658561 |
| mean anomaly at epoch: | 233.7780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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