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 37788U 26104.21234500 +.00000000 +00000-0 +89596-4 0 00007
2 37788 98.2762 0.3110 0033765 327.1907 184.6945 14.76415233 00
| Epoch (UTC): | 14 April 2026 05:05:46 |
| Eccentricity: | 0.0033765 |
| inclination: | 98.2762° |
| perigee height: | 617 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 0.3110° |
| argument of perigee: | 327.1907° |
| revolutions per day: | 14.76415233 |
| mean anomaly at epoch: | 184.6945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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