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 39451U 26079.93414473 +.00000000 +00000-0 +14282-3 0 00004
2 39451 87.7504 9.0849 0003455 79.9455 280.2184 15.27959141 00
| Epoch (UTC): | 20 March 2026 22:25:10 |
| Eccentricity: | 0.0003455 |
| inclination: | 87.7504° |
| perigee height: | 480 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 9.0849° |
| argument of perigee: | 79.9455° |
| revolutions per day: | 15.27959141 |
| mean anomaly at epoch: | 280.2184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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