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 26037.59960332 +.00000000 +00000-0 +89832-3 0 00000
2 23608 98.2886 237.4170 0007401 140.0235 220.1557 15.44728508 09
| Epoch (UTC): | 06 February 2026 14:23:25 |
| Eccentricity: | 0.0007401 |
| inclination: | 98.2886° |
| perigee height: | 427 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 237.4170° |
| argument of perigee: | 140.0235° |
| revolutions per day: | 15.44728508 |
| mean anomaly at epoch: | 220.1557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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