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 63274U 26145.34190270 +.00000000 +00000-0 +17151-2 0 00006
2 63274 42.9996 10.3089 0000460 1.2230 358.8638 15.70907654 07
| Epoch (UTC): | 25 May 2026 08:12:20 |
| Eccentricity: | 0.0000460 |
| inclination: | 42.9996° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 10.3089° |
| argument of perigee: | 1.2230° |
| revolutions per day: | 15.70907654 |
| mean anomaly at epoch: | 358.8638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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