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 66025U 26145.13596632 +.00000000 +00000-0 +65799-3 0 00004
2 66025 53.1576 108.5464 0001084 85.2334 274.8791 15.30217148 04
| Epoch (UTC): | 25 May 2026 03:15:47 |
| Eccentricity: | 0.0001084 |
| inclination: | 53.1576° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.5464° |
| argument of perigee: | 85.2334° |
| revolutions per day: | 15.30217148 |
| mean anomaly at epoch: | 274.8791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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