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 63670U 26145.39448709 +.00000000 +00000-0 +17375-2 0 00002
2 63670 43.0023 176.2307 0002145 260.9979 99.0646 15.70894249 09
| Epoch (UTC): | 25 May 2026 09:28:03 |
| Eccentricity: | 0.0002145 |
| inclination: | 43.0023° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 176.2307° |
| argument of perigee: | 260.9979° |
| revolutions per day: | 15.70894249 |
| mean anomaly at epoch: | 99.0646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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