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 64447U 26145.26343241 +.00000000 +00000-0 +68122-3 0 00003
2 64447 53.1584 93.0861 0001308 91.2039 268.9111 15.30213775 08
| Epoch (UTC): | 25 May 2026 06:19:20 |
| Eccentricity: | 0.0001308 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 93.0861° |
| argument of perigee: | 91.2039° |
| revolutions per day: | 15.30213775 |
| mean anomaly at epoch: | 268.9111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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