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 66632U 26145.27186066 +.00000000 +00000-0 +72293-3 0 00006
2 66632 53.1586 142.6697 0001048 81.5226 278.5896 15.34402143 07
| Epoch (UTC): | 25 May 2026 06:31:28 |
| Eccentricity: | 0.0001048 |
| inclination: | 53.1586° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 142.6697° |
| argument of perigee: | 81.5226° |
| revolutions per day: | 15.34402143 |
| mean anomaly at epoch: | 278.5896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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