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 23606U 26106.24314998 +.00000000 +00000-0 +26729-3 0 00004
2 23606 98.3205 315.4240 0007045 91.5953 268.6093 15.33382639 00
| Epoch (UTC): | 16 April 2026 05:50:08 |
| Eccentricity: | 0.0007045 |
| inclination: | 98.3205° |
| perigee height: | 461 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 315.4240° |
| argument of perigee: | 91.5953° |
| revolutions per day: | 15.33382639 |
| mean anomaly at epoch: | 268.6093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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