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 63494U 26145.41545044 +.00000000 +00000-0 +69322-3 0 00009
2 63494 53.1582 143.0719 0000882 66.9056 293.2043 15.42187462 00
| Epoch (UTC): | 25 May 2026 09:58:14 |
| Eccentricity: | 0.0000882 |
| inclination: | 53.1582° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.0719° |
| argument of perigee: | 66.9056° |
| revolutions per day: | 15.42187462 |
| mean anomaly at epoch: | 293.2043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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