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 63453U 26145.38636186 +.00000000 +00000-0 +22695-3 0 00000
2 63453 53.1593 146.4846 0001288 94.9560 265.1588 15.30209422 07
| Epoch (UTC): | 25 May 2026 09:16:21 |
| Eccentricity: | 0.0001288 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.4846° |
| argument of perigee: | 94.9560° |
| revolutions per day: | 15.30209422 |
| mean anomaly at epoch: | 265.1588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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