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 64134U 26145.30596029 +.00000000 +00000-0 +14847-2 0 00009
2 64134 43.0008 231.6005 0004282 292.8425 67.1991 15.70855543 06
| Epoch (UTC): | 25 May 2026 07:20:34 |
| Eccentricity: | 0.0004282 |
| inclination: | 43.0008° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 231.6005° |
| argument of perigee: | 292.8425° |
| revolutions per day: | 15.70855543 |
| mean anomaly at epoch: | 67.1991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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