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 58843U 26145.56346891 +.00000000 +00000-0 +15343-4 0 00001
2 58843 53.1590 207.4115 0001257 76.3072 283.8069 15.30187644 08
| Epoch (UTC): | 25 May 2026 13:31:23 |
| Eccentricity: | 0.0001257 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.4115° |
| argument of perigee: | 76.3072° |
| revolutions per day: | 15.30187644 |
| mean anomaly at epoch: | 283.8069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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