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 64210U 26145.13735941 +.00000000 +00000-0 +51607-3 0 00009
2 64210 53.1586 44.2680 0001134 86.5526 273.5605 15.30210067 01
| Epoch (UTC): | 25 May 2026 03:17:47 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.2680° |
| argument of perigee: | 86.5526° |
| revolutions per day: | 15.30210067 |
| mean anomaly at epoch: | 273.5605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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