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 64914U 26144.99658384 +.00000000 +00000-0 +41216-3 0 00003
2 64914 53.1573 351.4425 0000649 32.4086 327.6954 15.30204551 08
| Epoch (UTC): | 24 May 2026 23:55:04 |
| Eccentricity: | 0.0000649 |
| inclination: | 53.1573° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.4425° |
| argument of perigee: | 32.4086° |
| revolutions per day: | 15.30204551 |
| mean anomaly at epoch: | 327.6954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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