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 64371U 26145.59013647 +.00000000 +00000-0 +21129-2 0 00004
2 64371 43.0000 341.2925 0001938 259.3917 100.6733 15.70923890 07
| Epoch (UTC): | 25 May 2026 14:09:47 |
| Eccentricity: | 0.0001938 |
| inclination: | 43.0000° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 341.2925° |
| argument of perigee: | 259.3917° |
| revolutions per day: | 15.70923890 |
| mean anomaly at epoch: | 100.6733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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