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 63818U 26145.55171552 +.00000000 +00000-0 +56187-3 0 00008
2 63818 42.9988 98.1274 0000930 254.3584 105.7165 15.27584330 05
| Epoch (UTC): | 25 May 2026 13:14:28 |
| Eccentricity: | 0.0000930 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 98.1274° |
| argument of perigee: | 254.3584° |
| revolutions per day: | 15.27584330 |
| mean anomaly at epoch: | 105.7165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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