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 64277U 26145.36413016 +.00000000 +00000-0 +61330-3 0 00007
2 64277 53.1565 120.6663 0001303 95.9836 264.1313 15.30213172 09
| Epoch (UTC): | 25 May 2026 08:44:20 |
| Eccentricity: | 0.0001303 |
| inclination: | 53.1565° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.6663° |
| argument of perigee: | 95.9836° |
| revolutions per day: | 15.30213172 |
| mean anomaly at epoch: | 264.1313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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