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 23908U 26088.20332308 +.00000000 +00000-0 +63390-3 0 00004
2 23908 63.3214 40.8745 0847504 48.2447 318.7936 13.45980910 05
| Epoch (UTC): | 29 March 2026 04:52:47 |
| Eccentricity: | 0.0847504 |
| inclination: | 63.3214° |
| perigee height: | 454 km |
| apogee height: | 1720 km |
| right ascension of ascending node: | 40.8745° |
| argument of perigee: | 48.2447° |
| revolutions per day: | 13.45980910 |
| mean anomaly at epoch: | 318.7936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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