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 58829U 26145.41913215 +.00000000 +00000-0 +14410-3 0 00002
2 58829 53.1593 207.9321 0001253 89.2898 270.8246 15.30182537 03
| Epoch (UTC): | 25 May 2026 10:03:33 |
| Eccentricity: | 0.0001253 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.9321° |
| argument of perigee: | 89.2898° |
| revolutions per day: | 15.30182537 |
| mean anomaly at epoch: | 270.8246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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