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 64181U 26145.23976766 +.00000000 +00000-0 +28444-3 0 00002
2 64181 53.1591 95.6762 0001047 103.1348 256.9770 15.30197568 04
| Epoch (UTC): | 25 May 2026 05:45:15 |
| Eccentricity: | 0.0001047 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.6762° |
| argument of perigee: | 103.1348° |
| revolutions per day: | 15.30197568 |
| mean anomaly at epoch: | 256.9770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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