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 63654U 26145.11878744 +.00000000 +00000-0 +65545-3 0 00003
2 63654 43.0018 293.7515 0001109 271.0951 88.9773 15.27573487 01
| Epoch (UTC): | 25 May 2026 02:51:03 |
| Eccentricity: | 0.0001109 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 293.7515° |
| argument of perigee: | 271.0951° |
| revolutions per day: | 15.27573487 |
| mean anomaly at epoch: | 88.9773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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