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 26072.87258977 +.00000000 +00000-0 +82044-3 0 00003
2 23608 98.2877 277.7133 0007187 22.5737 337.5826 15.47553058 08
| Epoch (UTC): | 13 March 2026 20:56:31 |
| Eccentricity: | 0.0007187 |
| inclination: | 98.2877° |
| perigee height: | 419 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 277.7133° |
| argument of perigee: | 22.5737° |
| revolutions per day: | 15.47553058 |
| mean anomaly at epoch: | 337.5826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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