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 51637U 26145.36722948 +.00000000 +00000-0 +41217-4 0 00003
2 51637 87.9153 10.4178 0002076 77.3945 282.7419 13.17650787 06
| Epoch (UTC): | 25 May 2026 08:48:48 |
| Eccentricity: | 0.0002076 |
| inclination: | 87.9153° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4178° |
| argument of perigee: | 77.3945° |
| revolutions per day: | 13.17650787 |
| mean anomaly at epoch: | 282.7419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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