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 59307U 26145.52659575 +.00000000 +00000-0 -33268-5 0 00007
2 59307 43.0006 156.9365 0001190 274.8592 85.2124 15.27573386 01
| Epoch (UTC): | 25 May 2026 12:38:17 |
| Eccentricity: | 0.0001190 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 156.9365° |
| argument of perigee: | 274.8592° |
| revolutions per day: | 15.27573386 |
| mean anomaly at epoch: | 85.2124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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