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 26134.85668163 +.00000000 +00000-0 +11254-3 0 00000
2 23908 63.3191 278.8228 0849673 48.9764 318.1619 13.46163949 04
| Epoch (UTC): | 14 May 2026 20:33:37 |
| Eccentricity: | 0.0849673 |
| inclination: | 63.3191° |
| perigee height: | 452 km |
| apogee height: | 1721 km |
| right ascension of ascending node: | 278.8228° |
| argument of perigee: | 48.9764° |
| revolutions per day: | 13.46163949 |
| mean anomaly at epoch: | 318.1619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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