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 66016U 26145.31514022 +.00000000 +00000-0 +41812-3 0 00007
2 66016 53.1576 108.2467 0001258 93.8061 266.3083 15.30205604 03
| Epoch (UTC): | 25 May 2026 07:33:48 |
| Eccentricity: | 0.0001258 |
| inclination: | 53.1576° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.2467° |
| argument of perigee: | 93.8061° |
| revolutions per day: | 15.30205604 |
| mean anomaly at epoch: | 266.3083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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