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 66375U 26145.61611141 +.00000000 +00000-0 +41852-3 0 00002
2 66375 53.1585 232.2353 0001170 90.0689 270.0446 15.30206440 05
| Epoch (UTC): | 25 May 2026 14:47:12 |
| Eccentricity: | 0.0001170 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.2353° |
| argument of perigee: | 90.0689° |
| revolutions per day: | 15.30206440 |
| mean anomaly at epoch: | 270.0446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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