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 58735U 26145.36890066 +.00000000 +00000-0 +30991-4 0 00003
2 58735 43.0022 146.4610 0001247 272.9997 87.0712 15.27575809 06
| Epoch (UTC): | 25 May 2026 08:51:13 |
| Eccentricity: | 0.0001247 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.4610° |
| argument of perigee: | 272.9997° |
| revolutions per day: | 15.27575809 |
| mean anomaly at epoch: | 87.0712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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