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 64306U 26145.32838948 +.00000000 +00000-0 +14047-3 0 00004
2 64306 70.0023 1.4059 0002828 267.4821 92.6015 14.98335742 01
| Epoch (UTC): | 25 May 2026 07:52:52 |
| Eccentricity: | 0.0002828 |
| inclination: | 70.0023° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.4059° |
| argument of perigee: | 267.4821° |
| revolutions per day: | 14.98335742 |
| mean anomaly at epoch: | 92.6015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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