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 64376U 26145.56889840 +.00000000 +00000-0 +13309-2 0 00003
2 64376 42.9995 341.1181 0001465 241.3489 118.7231 15.70950930 04
| Epoch (UTC): | 25 May 2026 13:39:12 |
| Eccentricity: | 0.0001465 |
| inclination: | 42.9995° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 341.1181° |
| argument of perigee: | 241.3489° |
| revolutions per day: | 15.70950930 |
| mean anomaly at epoch: | 118.7231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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