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 66633U 26145.40424123 +.00000000 +00000-0 +72909-3 0 00005
2 66633 53.1587 142.0783 0001470 98.3793 261.7376 15.34377633 05
| Epoch (UTC): | 25 May 2026 09:42:06 |
| Eccentricity: | 0.0001470 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 142.0783° |
| argument of perigee: | 98.3793° |
| revolutions per day: | 15.34377633 |
| mean anomaly at epoch: | 261.7376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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