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 23608U 26039.80192301 +.00000000 +00000-0 +75285-3 0 00006
2 23608 98.2892 239.9281 0007439 132.3569 227.8308 15.44897633 05
| Epoch (UTC): | 08 February 2026 19:14:46 |
| Eccentricity: | 0.0007439 |
| inclination: | 98.2892° |
| perigee height: | 427 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 239.9281° |
| argument of perigee: | 132.3569° |
| revolutions per day: | 15.44897633 |
| mean anomaly at epoch: | 227.8308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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