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 59771U 26145.38129324 +.00000000 +00000-0 -17990-6 0 00005
2 59771 53.1618 30.8440 0001205 94.5595 265.5544 15.30191564 05
| Epoch (UTC): | 25 May 2026 09:09:03 |
| Eccentricity: | 0.0001205 |
| inclination: | 53.1618° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.8440° |
| argument of perigee: | 94.5595° |
| revolutions per day: | 15.30191564 |
| mean anomaly at epoch: | 265.5544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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