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 64304U 26145.31586617 +.00000000 +00000-0 +15998-2 0 00009
2 64304 70.0061 1.3625 0001391 54.9178 305.2111 14.98375641 09
| Epoch (UTC): | 25 May 2026 07:34:50 |
| Eccentricity: | 0.0001391 |
| inclination: | 70.0061° |
| perigee height: | 571 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 1.3625° |
| argument of perigee: | 54.9178° |
| revolutions per day: | 14.98375641 |
| mean anomaly at epoch: | 305.2111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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