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 63741U 26145.61336632 +.00000000 +00000-0 +51262-4 0 00002
2 63741 51.9000 112.8942 0000691 64.0349 296.0685 14.79938853 00
| Epoch (UTC): | 25 May 2026 14:43:14 |
| Eccentricity: | 0.0000691 |
| inclination: | 51.9000° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 112.8942° |
| argument of perigee: | 64.0349° |
| revolutions per day: | 14.79938853 |
| mean anomaly at epoch: | 296.0685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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