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 51774U 26145.56605166 +.00000000 +00000-0 +36784-4 0 00002
2 51774 53.2131 354.0092 0001515 89.7937 270.3229 15.08837383 00
| Epoch (UTC): | 25 May 2026 13:35:06 |
| Eccentricity: | 0.0001515 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 354.0092° |
| argument of perigee: | 89.7937° |
| revolutions per day: | 15.08837383 |
| mean anomaly at epoch: | 270.3229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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