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 61714U 26145.28711801 +.00000000 +00000-0 +20930-4 0 00006
2 61714 53.1602 105.5762 0001302 85.9605 274.1545 15.30191363 03
| Epoch (UTC): | 25 May 2026 06:53:26 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 105.5762° |
| argument of perigee: | 85.9605° |
| revolutions per day: | 15.30191363 |
| mean anomaly at epoch: | 274.1545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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