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 64195U 26145.27766709 +.00000000 +00000-0 +70677-3 0 00000
2 64195 53.1577 95.2028 0001162 91.1426 268.9707 15.30199710 09
| Epoch (UTC): | 25 May 2026 06:39:50 |
| Eccentricity: | 0.0001162 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.2028° |
| argument of perigee: | 91.1426° |
| revolutions per day: | 15.30199710 |
| mean anomaly at epoch: | 268.9707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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