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 63674U 26145.56400017 +.00000000 +00000-0 +13936-2 0 00004
2 63674 43.0005 174.9097 0001134 254.5825 105.4918 15.70864907 02
| Epoch (UTC): | 25 May 2026 13:32:09 |
| Eccentricity: | 0.0001134 |
| inclination: | 43.0005° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 174.9097° |
| argument of perigee: | 254.5825° |
| revolutions per day: | 15.70864907 |
| mean anomaly at epoch: | 105.4918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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