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 63667U 26145.47399787 +.00000000 +00000-0 +13510-2 0 00005
2 63667 42.9996 175.9785 0001741 255.5129 104.5546 15.70833386 02
| Epoch (UTC): | 25 May 2026 11:22:33 |
| Eccentricity: | 0.0001741 |
| inclination: | 42.9996° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 175.9785° |
| argument of perigee: | 255.5129° |
| revolutions per day: | 15.70833386 |
| mean anomaly at epoch: | 104.5546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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