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 58030U 26145.24025360 +.00000000 +00000-0 +35938-4 0 00001
2 58030 53.1605 82.8090 0001259 84.3308 275.7837 15.30201450 08
| Epoch (UTC): | 25 May 2026 05:45:57 |
| Eccentricity: | 0.0001259 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 82.8090° |
| argument of perigee: | 84.3308° |
| revolutions per day: | 15.30201450 |
| mean anomaly at epoch: | 275.7837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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