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 26069.51000161 +.00000000 +00000-0 +83589-3 0 00005
2 23608 98.2877 273.8647 0007335 34.1509 326.0209 15.47273741 02
| Epoch (UTC): | 10 March 2026 12:14:24 |
| Eccentricity: | 0.0007335 |
| inclination: | 98.2877° |
| perigee height: | 420 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 273.8647° |
| argument of perigee: | 34.1509° |
| revolutions per day: | 15.47273741 |
| mean anomaly at epoch: | 326.0209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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