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 64539U 26145.56619394 +.00000000 +00000-0 +16225-3 0 00000
2 64539 97.4705 261.2132 0001909 240.1542 119.9505 15.22676213 00
| Epoch (UTC): | 25 May 2026 13:35:19 |
| Eccentricity: | 0.0001909 |
| inclination: | 97.4705° |
| perigee height: | 496 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 261.2132° |
| argument of perigee: | 240.1542° |
| revolutions per day: | 15.22676213 |
| mean anomaly at epoch: | 119.9505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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