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 54076U 26145.01640672 +.00000000 +00000-0 +26495-4 0 00009
2 54076 53.2151 1.6782 0001439 83.6985 276.4171 15.08841647 03
| Epoch (UTC): | 25 May 2026 00:23:37 |
| Eccentricity: | 0.0001439 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 1.6782° |
| argument of perigee: | 83.6985° |
| revolutions per day: | 15.08841647 |
| mean anomaly at epoch: | 276.4171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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