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 66623U 26145.39792538 +.00000000 +00000-0 +10184-2 0 00006
2 66623 53.1595 142.0357 0001402 87.5595 272.5568 15.34403433 06
| Epoch (UTC): | 25 May 2026 09:33:00 |
| Eccentricity: | 0.0001402 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 142.0357° |
| argument of perigee: | 87.5595° |
| revolutions per day: | 15.34403433 |
| mean anomaly at epoch: | 272.5568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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