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 59770U 26145.10631416 +.00000000 +00000-0 +39451-4 0 00007
2 59770 53.1612 31.9746 0001169 70.5988 289.5139 15.30193967 03
| Epoch (UTC): | 25 May 2026 02:33:05 |
| Eccentricity: | 0.0001169 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 31.9746° |
| argument of perigee: | 70.5988° |
| revolutions per day: | 15.30193967 |
| mean anomaly at epoch: | 289.5139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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