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 64315U 26145.34906794 +.00000000 +00000-0 +23873-3 0 00008
2 64315 70.0018 1.0804 0002675 269.1062 90.9790 14.98336474 09
| Epoch (UTC): | 25 May 2026 08:22:39 |
| Eccentricity: | 0.0002675 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.0804° |
| argument of perigee: | 269.1062° |
| revolutions per day: | 14.98336474 |
| mean anomaly at epoch: | 90.9790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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