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 58998U 26145.21486124 +.00000000 +00000-0 +12082-3 0 00004
2 58998 53.1593 82.3971 0001036 82.6405 277.4713 15.30220355 09
| Epoch (UTC): | 25 May 2026 05:09:24 |
| Eccentricity: | 0.0001036 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 82.3971° |
| argument of perigee: | 82.6405° |
| revolutions per day: | 15.30220355 |
| mean anomaly at epoch: | 277.4713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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