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 64024U 26145.65690506 +.00000000 +00000-0 +21484-3 0 00006
2 64024 70.0002 280.2875 0002840 269.3880 90.6953 14.98335385 00
| Epoch (UTC): | 25 May 2026 15:45:56 |
| Eccentricity: | 0.0002840 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 280.2875° |
| argument of perigee: | 269.3880° |
| revolutions per day: | 14.98335385 |
| mean anomaly at epoch: | 90.6953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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