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 64428U 26145.43112804 +.00000000 +00000-0 +26464-3 0 00003
2 64428 70.0005 240.9148 0003510 270.0265 90.0491 14.98336788 07
| Epoch (UTC): | 25 May 2026 10:20:49 |
| Eccentricity: | 0.0003510 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.9148° |
| argument of perigee: | 270.0265° |
| revolutions per day: | 14.98336788 |
| mean anomaly at epoch: | 90.0491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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