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 66824U 26145.39661899 +.00000000 +00000-0 +35154-3 0 00009
2 66824 70.0004 141.1433 0003258 271.0242 89.0544 14.98335277 01
| Epoch (UTC): | 25 May 2026 09:31:07 |
| Eccentricity: | 0.0003258 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 141.1433° |
| argument of perigee: | 271.0242° |
| revolutions per day: | 14.98335277 |
| mean anomaly at epoch: | 89.0544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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