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 66839U 26145.44682448 +.00000000 +00000-0 +22437-3 0 00004
2 66839 70.0005 140.9127 0004072 265.3052 94.7642 14.98335736 07
| Epoch (UTC): | 25 May 2026 10:43:25 |
| Eccentricity: | 0.0004072 |
| inclination: | 70.0005° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 140.9127° |
| argument of perigee: | 265.3052° |
| revolutions per day: | 14.98335736 |
| mean anomaly at epoch: | 94.7642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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