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 65811U 26145.32662256 +.00000000 +00000-0 -26008-4 0 00005
2 65811 97.4491 8.1462 0002738 90.4125 269.7416 15.05657835 09
| Epoch (UTC): | 25 May 2026 07:50:20 |
| Eccentricity: | 0.0002738 |
| inclination: | 97.4491° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.1462° |
| argument of perigee: | 90.4125° |
| revolutions per day: | 15.05657835 |
| mean anomaly at epoch: | 269.7416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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