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 51638U 26145.41781375 +.00000000 +00000-0 -12160-2 0 00003
2 51638 87.8848 40.8003 0001964 77.2047 282.9300 13.10370926 06
| Epoch (UTC): | 25 May 2026 10:01:39 |
| Eccentricity: | 0.0001964 |
| inclination: | 87.8848° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8003° |
| argument of perigee: | 77.2047° |
| revolutions per day: | 13.10370926 |
| mean anomaly at epoch: | 282.9300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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