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 64170U 26145.12419203 +.00000000 +00000-0 +41518-3 0 00003
2 64170 53.1591 95.6814 0001562 53.6185 306.4960 15.31711657 04
| Epoch (UTC): | 25 May 2026 02:58:50 |
| Eccentricity: | 0.0001562 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.6814° |
| argument of perigee: | 53.6185° |
| revolutions per day: | 15.31711657 |
| mean anomaly at epoch: | 306.4960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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