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 66363U 26145.25547567 +.00000000 +00000-0 +83479-3 0 00000
2 66363 53.1594 237.1369 0001580 92.8821 267.2360 15.30215776 01
| Epoch (UTC): | 25 May 2026 06:07:53 |
| Eccentricity: | 0.0001580 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 237.1369° |
| argument of perigee: | 92.8821° |
| revolutions per day: | 15.30215776 |
| mean anomaly at epoch: | 267.2360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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