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 63247U 26145.65789132 +.00000000 +00000-0 +40878-3 0 00004
2 63247 97.6935 38.1800 0001054 300.8925 59.2193 14.97114616 09
| Epoch (UTC): | 25 May 2026 15:47:21 |
| Eccentricity: | 0.0001054 |
| inclination: | 97.6935° |
| perigee height: | 575 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 38.1800° |
| argument of perigee: | 300.8925° |
| revolutions per day: | 14.97114616 |
| mean anomaly at epoch: | 59.2193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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