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 66337U 26145.34941134 +.00000000 +00000-0 +51081-3 0 00003
2 66337 43.0011 140.0004 0001524 279.0350 81.0329 15.27594579 00
| Epoch (UTC): | 25 May 2026 08:23:09 |
| Eccentricity: | 0.0001524 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 140.0004° |
| argument of perigee: | 279.0350° |
| revolutions per day: | 15.27594579 |
| mean anomaly at epoch: | 81.0329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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