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 58702U 26145.59098119 +.00000000 +00000-0 +20746-3 0 00007
2 58702 97.4650 331.5203 0007103 81.6754 278.5290 15.26476354 00
| Epoch (UTC): | 25 May 2026 14:11:00 |
| Eccentricity: | 0.0007103 |
| inclination: | 97.4650° |
| perigee height: | 481 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 331.5203° |
| argument of perigee: | 81.6754° |
| revolutions per day: | 15.26476354 |
| mean anomaly at epoch: | 278.5290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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