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 51992U 26145.10972074 +.00000000 +00000-0 -29361-3 0 00002
2 51992 53.2147 36.0566 0001736 96.2096 263.9094 15.08865567 09
| Epoch (UTC): | 25 May 2026 02:37:59 |
| Eccentricity: | 0.0001736 |
| inclination: | 53.2147° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 36.0566° |
| argument of perigee: | 96.2096° |
| revolutions per day: | 15.08865567 |
| mean anomaly at epoch: | 263.9094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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