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 58999U 26145.54357056 +.00000000 +00000-0 -24781-5 0 00004
2 58999 53.1610 80.8846 0002175 95.1890 264.9359 15.30189525 06
| Epoch (UTC): | 25 May 2026 13:02:44 |
| Eccentricity: | 0.0002175 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 80.8846° |
| argument of perigee: | 95.1890° |
| revolutions per day: | 15.30189525 |
| mean anomaly at epoch: | 264.9359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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