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 64605U 26145.56661190 +.00000000 +00000-0 +75443-3 0 00002
2 64605 53.1590 337.5471 0001464 93.4708 266.6461 15.31704708 09
| Epoch (UTC): | 25 May 2026 13:35:55 |
| Eccentricity: | 0.0001464 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 337.5471° |
| argument of perigee: | 93.4708° |
| revolutions per day: | 15.31704708 |
| mean anomaly at epoch: | 266.6461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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