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 65771U 26145.49847395 +.00000000 +00000-0 +39009-3 0 00000
2 65771 51.9022 63.4620 0001145 80.4589 279.6503 14.79942451 01
| Epoch (UTC): | 25 May 2026 11:57:48 |
| Eccentricity: | 0.0001145 |
| inclination: | 51.9022° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 63.4620° |
| argument of perigee: | 80.4589° |
| revolutions per day: | 14.79942451 |
| mean anomaly at epoch: | 279.6503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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