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 66682U 26145.45928543 +.00000000 +00000-0 +65930-4 0 00006
2 66682 97.5294 216.9543 0003414 237.6938 122.3954 14.97484518 03
| Epoch (UTC): | 25 May 2026 11:01:22 |
| Eccentricity: | 0.0003414 |
| inclination: | 97.5294° |
| perigee height: | 572 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 216.9543° |
| argument of perigee: | 237.6938° |
| revolutions per day: | 14.97484518 |
| mean anomaly at epoch: | 122.3954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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