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 66903U 26145.10252030 +.00000000 +00000-0 +74425-3 0 00003
2 66903 53.1579 29.2088 0000557 81.2631 278.8433 15.30205972 02
| Epoch (UTC): | 25 May 2026 02:27:37 |
| Eccentricity: | 0.0000557 |
| inclination: | 53.1579° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.2088° |
| argument of perigee: | 81.2631° |
| revolutions per day: | 15.30205972 |
| mean anomaly at epoch: | 278.8433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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