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 66634U 26145.26134080 +.00000000 +00000-0 +83564-3 0 00009
2 66634 53.1592 142.5995 0001191 102.6892 257.4244 15.34404313 03
| Epoch (UTC): | 25 May 2026 06:16:19 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 142.5995° |
| argument of perigee: | 102.6892° |
| revolutions per day: | 15.34404313 |
| mean anomaly at epoch: | 257.4244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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