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 61209U 26145.28746458 +.00000000 +00000-0 +14918-4 0 00000
2 61209 53.1590 158.3391 0000776 94.8929 265.2178 15.69712323 04
| Epoch (UTC): | 25 May 2026 06:53:56 |
| Eccentricity: | 0.0000776 |
| inclination: | 53.1590° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 158.3391° |
| argument of perigee: | 94.8929° |
| revolutions per day: | 15.69712323 |
| mean anomaly at epoch: | 265.2178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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