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 66971U 26145.16649961 +.00000000 +00000-0 +60314-3 0 00009
2 66971 43.0023 311.5413 0002326 265.9181 94.1405 15.27578050 09
| Epoch (UTC): | 25 May 2026 03:59:45 |
| Eccentricity: | 0.0002326 |
| inclination: | 43.0023° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 311.5413° |
| argument of perigee: | 265.9181° |
| revolutions per day: | 15.27578050 |
| mean anomaly at epoch: | 94.1405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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