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 53174U 26145.39266628 +.00000000 +00000-0 +99286-4 0 00001
2 53174 53.2128 189.7220 0001587 84.7896 275.3277 15.08847040 05
| Epoch (UTC): | 25 May 2026 09:25:26 |
| Eccentricity: | 0.0001587 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 189.7220° |
| argument of perigee: | 84.7896° |
| revolutions per day: | 15.08847040 |
| mean anomaly at epoch: | 275.3277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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