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 64025U 26145.43177080 +.00000000 +00000-0 +31261-3 0 00004
2 64025 70.0009 281.1050 0003118 268.0210 92.0592 14.98335673 00
| Epoch (UTC): | 25 May 2026 10:21:44 |
| Eccentricity: | 0.0003118 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.1050° |
| argument of perigee: | 268.0210° |
| revolutions per day: | 14.98335673 |
| mean anomaly at epoch: | 92.0592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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