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 31792U 26046.02184367 +.00000000 +00000-0 +17135-3 0 00004
2 31792 70.9399 250.9260 0007795 302.7740 57.2630 14.12937059 00
| Epoch (UTC): | 15 February 2026 00:31:27 |
| Eccentricity: | 0.0007795 |
| inclination: | 70.9399° |
| perigee height: | 844 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 250.9260° |
| argument of perigee: | 302.7740° |
| revolutions per day: | 14.12937059 |
| mean anomaly at epoch: | 57.2630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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