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 64262U 26145.63699833 +.00000000 +00000-0 +35426-3 0 00001
2 64262 53.1582 119.5233 0001119 94.9601 265.1528 15.30204369 03
| Epoch (UTC): | 25 May 2026 15:17:16 |
| Eccentricity: | 0.0001119 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 119.5233° |
| argument of perigee: | 94.9601° |
| revolutions per day: | 15.30204369 |
| mean anomaly at epoch: | 265.1528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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