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 66107U 26145.62376030 +.00000000 +00000-0 +56313-3 0 00009
2 66107 53.1596 106.5079 0001584 100.3410 259.7769 15.30201072 02
| Epoch (UTC): | 25 May 2026 14:58:12 |
| Eccentricity: | 0.0001584 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.5079° |
| argument of perigee: | 100.3410° |
| revolutions per day: | 15.30201072 |
| mean anomaly at epoch: | 259.7769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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