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 64248U 26145.55038751 +.00000000 +00000-0 +43909-3 0 00007
2 64248 43.0021 233.0232 0000289 308.1237 51.9588 15.27590341 07
| Epoch (UTC): | 25 May 2026 13:12:33 |
| Eccentricity: | 0.0000289 |
| inclination: | 43.0021° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 233.0232° |
| argument of perigee: | 308.1237° |
| revolutions per day: | 15.27590341 |
| mean anomaly at epoch: | 51.9588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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