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 64087U 26145.64511947 +.00000000 +00000-0 +24192-3 0 00004
2 64087 97.4770 220.7023 0003424 49.4632 310.6899 15.15949747 06
| Epoch (UTC): | 25 May 2026 15:28:58 |
| Eccentricity: | 0.0003424 |
| inclination: | 97.4770° |
| perigee height: | 516 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 220.7023° |
| argument of perigee: | 49.4632° |
| revolutions per day: | 15.15949747 |
| mean anomaly at epoch: | 310.6899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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