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 63514U 26145.28989954 +.00000000 +00000-0 +48888-3 0 00003
2 63514 53.1560 144.3712 0001092 86.8863 273.2262 15.30206630 04
| Epoch (UTC): | 25 May 2026 06:57:27 |
| Eccentricity: | 0.0001092 |
| inclination: | 53.1560° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.3712° |
| argument of perigee: | 86.8863° |
| revolutions per day: | 15.30206630 |
| mean anomaly at epoch: | 273.2262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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