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 66823U 26145.42997543 +.00000000 +00000-0 +15868-3 0 00000
2 66823 70.0007 140.8558 0004148 252.7852 107.2854 14.98323290 08
| Epoch (UTC): | 25 May 2026 10:19:09 |
| Eccentricity: | 0.0004148 |
| inclination: | 70.0007° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 140.8558° |
| argument of perigee: | 252.7852° |
| revolutions per day: | 14.98323290 |
| mean anomaly at epoch: | 107.2854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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