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 61210U 26145.28266303 +.00000000 +00000-0 +71819-5 0 00002
2 61210 53.1591 159.0357 0000892 132.4434 227.6660 15.69707027 09
| Epoch (UTC): | 25 May 2026 06:47:02 |
| Eccentricity: | 0.0000892 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 159.0357° |
| argument of perigee: | 132.4434° |
| revolutions per day: | 15.69707027 |
| mean anomaly at epoch: | 227.6660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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