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 26040.25531116 +.00000000 +00000-0 +82272-3 0 00002
2 23608 98.2893 240.4452 0007437 130.7407 229.4485 15.44934711 07
| Epoch (UTC): | 09 February 2026 06:07:38 |
| Eccentricity: | 0.0007437 |
| inclination: | 98.2893° |
| perigee height: | 427 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 240.4452° |
| argument of perigee: | 130.7407° |
| revolutions per day: | 15.44934711 |
| mean anomaly at epoch: | 229.4485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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