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 23607U 26087.90880944 +.00000000 +00000-0 +17623-3 0 00008
2 23607 98.2988 56.0666 0006617 64.9656 295.2244 14.84606591 01
| Epoch (UTC): | 28 March 2026 21:48:41 |
| Eccentricity: | 0.0006617 |
| inclination: | 98.2988° |
| perigee height: | 610 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 56.0666° |
| argument of perigee: | 64.9656° |
| revolutions per day: | 14.84606591 |
| mean anomaly at epoch: | 295.2244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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