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 64128U 26145.58684042 +.00000000 +00000-0 +99787-3 0 00002
2 64128 43.0004 230.2820 0001528 266.6294 93.4399 15.70863010 00
| Epoch (UTC): | 25 May 2026 14:05:03 |
| Eccentricity: | 0.0001528 |
| inclination: | 43.0004° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 230.2820° |
| argument of perigee: | 266.6294° |
| revolutions per day: | 15.70863010 |
| mean anomaly at epoch: | 93.4399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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