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 51642U 26145.42611272 +.00000000 +00000-0 -19541-2 0 00007
2 51642 87.8851 40.7967 0002229 83.1814 276.9567 13.10372397 08
| Epoch (UTC): | 25 May 2026 10:13:36 |
| Eccentricity: | 0.0002229 |
| inclination: | 87.8851° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7967° |
| argument of perigee: | 83.1814° |
| revolutions per day: | 13.10372397 |
| mean anomaly at epoch: | 276.9567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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