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 59669U 26145.52324554 +.00000000 +00000-0 +11714-3 0 00003
2 59669 42.9991 327.8896 0001079 269.6192 90.4536 15.27582322 00
| Epoch (UTC): | 25 May 2026 12:33:28 |
| Eccentricity: | 0.0001079 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.8896° |
| argument of perigee: | 269.6192° |
| revolutions per day: | 15.27582322 |
| mean anomaly at epoch: | 90.4536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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