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 66196U 26145.56253448 +.00000000 +00000-0 +73142-3 0 00006
2 66196 53.1582 248.1656 0001694 95.4432 264.6762 15.30212937 09
| Epoch (UTC): | 25 May 2026 13:30:02 |
| Eccentricity: | 0.0001694 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.1656° |
| argument of perigee: | 95.4432° |
| revolutions per day: | 15.30212937 |
| mean anomaly at epoch: | 264.6762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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