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 63567U 26145.41897828 +.00000000 +00000-0 +48002-3 0 00002
2 63567 42.9989 197.1465 0001651 268.7516 91.3147 15.27593252 07
| Epoch (UTC): | 25 May 2026 10:03:19 |
| Eccentricity: | 0.0001651 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.1465° |
| argument of perigee: | 268.7516° |
| revolutions per day: | 15.27593252 |
| mean anomaly at epoch: | 91.3147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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