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 51633U 26145.12762062 +.00000000 +00000-0 +57811-5 0 00002
2 51633 87.9161 10.4298 0001683 78.4707 281.6614 13.17649290 07
| Epoch (UTC): | 25 May 2026 03:03:46 |
| Eccentricity: | 0.0001683 |
| inclination: | 87.9161° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4298° |
| argument of perigee: | 78.4707° |
| revolutions per day: | 13.17649290 |
| mean anomaly at epoch: | 281.6614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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