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 23317U 26073.46947130 +.00000000 +00000-0 +18417-3 0 00005
2 23317 82.5374 345.4526 0014912 229.4458 130.5467 14.96908156 02
| Epoch (UTC): | 14 March 2026 11:16:02 |
| Eccentricity: | 0.0014912 |
| inclination: | 82.5374° |
| perigee height: | 566 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 345.4526° |
| argument of perigee: | 229.4458° |
| revolutions per day: | 14.96908156 |
| mean anomaly at epoch: | 130.5467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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