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 23893U 26140.33054044 +.00000000 +00000-0 +10373-3 0 00001
2 23893 63.3194 264.9987 0849694 48.7559 318.3577 13.46168845 06
| Epoch (UTC): | 20 May 2026 07:55:58 |
| Eccentricity: | 0.0849694 |
| inclination: | 63.3194° |
| perigee height: | 452 km |
| apogee height: | 1721 km |
| right ascension of ascending node: | 264.9987° |
| argument of perigee: | 48.7559° |
| revolutions per day: | 13.46168845 |
| mean anomaly at epoch: | 318.3577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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