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 64439U 26145.24463503 +.00000000 +00000-0 +50904-3 0 00005
2 64439 53.1601 92.2653 0001153 86.2246 273.8889 15.34406996 01
| Epoch (UTC): | 25 May 2026 05:52:16 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.2653° |
| argument of perigee: | 86.2246° |
| revolutions per day: | 15.34406996 |
| mean anomaly at epoch: | 273.8889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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