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 43262U 26145.61697478 +.00000000 +00000-0 +18275-3 0 00002
2 43262 98.0536 208.2543 0002017 107.6107 252.5323 14.76442752 00
| Epoch (UTC): | 25 May 2026 14:48:26 |
| Eccentricity: | 0.0002017 |
| inclination: | 98.0536° |
| perigee height: | 639 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 208.2543° |
| argument of perigee: | 107.6107° |
| revolutions per day: | 14.76442752 |
| mean anomaly at epoch: | 252.5323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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