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 66929U 26145.62111910 +.00000000 +00000-0 +65394-3 0 00004
2 66929 53.1606 0.5242 0001113 95.3892 264.7237 15.34408829 05
| Epoch (UTC): | 25 May 2026 14:54:24 |
| Eccentricity: | 0.0001113 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 0.5242° |
| argument of perigee: | 95.3892° |
| revolutions per day: | 15.34408829 |
| mean anomaly at epoch: | 264.7237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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