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 58047U 26145.46861176 +.00000000 +00000-0 -56171-4 0 00009
2 58047 53.1602 171.8465 0001411 73.4583 286.6573 15.30204856 03
| Epoch (UTC): | 25 May 2026 11:14:48 |
| Eccentricity: | 0.0001411 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.8465° |
| argument of perigee: | 73.4583° |
| revolutions per day: | 15.30204856 |
| mean anomaly at epoch: | 286.6573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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