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 59353U 26145.57163022 +.00000000 +00000-0 +16689-4 0 00006
2 59353 43.0028 185.4424 0001692 288.6573 71.4095 15.27580761 07
| Epoch (UTC): | 25 May 2026 13:43:08 |
| Eccentricity: | 0.0001692 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.4424° |
| argument of perigee: | 288.6573° |
| revolutions per day: | 15.27580761 |
| mean anomaly at epoch: | 71.4095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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