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 61724U 26145.12072080 +.00000000 +00000-0 +33382-4 0 00004
2 61724 53.1605 106.6733 0001380 99.9183 260.1973 15.30191631 07
| Epoch (UTC): | 25 May 2026 02:53:50 |
| Eccentricity: | 0.0001380 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.6733° |
| argument of perigee: | 99.9183° |
| revolutions per day: | 15.30191631 |
| mean anomaly at epoch: | 260.1973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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