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 58357U 26145.05738824 +.00000000 +00000-0 +11094-2 0 00003
2 58357 43.0106 265.8303 0004074 305.3416 54.7055 15.27005593 01
| Epoch (UTC): | 25 May 2026 01:22:38 |
| Eccentricity: | 0.0004074 |
| inclination: | 43.0106° |
| perigee height: | 482 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 265.8303° |
| argument of perigee: | 305.3416° |
| revolutions per day: | 15.27005593 |
| mean anomaly at epoch: | 54.7055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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