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 64048U 26145.31876256 +.00000000 +00000-0 +67321-4 0 00004
2 64048 97.4118 218.3033 0001598 89.4944 270.6473 15.19180542 00
| Epoch (UTC): | 25 May 2026 07:39:01 |
| Eccentricity: | 0.0001598 |
| inclination: | 97.4118° |
| perigee height: | 507 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 218.3033° |
| argument of perigee: | 89.4944° |
| revolutions per day: | 15.19180542 |
| mean anomaly at epoch: | 270.6473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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