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 63447U 26145.32210277 +.00000000 +00000-0 +43691-3 0 00005
2 63447 53.1590 146.7965 0001189 88.9217 271.1920 15.30205649 08
| Epoch (UTC): | 25 May 2026 07:43:49 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.7965° |
| argument of perigee: | 88.9217° |
| revolutions per day: | 15.30205649 |
| mean anomaly at epoch: | 271.1920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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