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 64724U 26145.42168104 +.00000000 +00000-0 +37560-3 0 00004
2 64724 53.1590 184.3633 0001120 90.9062 269.2067 15.30205821 05
| Epoch (UTC): | 25 May 2026 10:07:13 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.3633° |
| argument of perigee: | 90.9062° |
| revolutions per day: | 15.30205821 |
| mean anomaly at epoch: | 269.2067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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