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 51132U 26145.18333037 +.00000000 +00000-0 +36810-4 0 00003
2 51132 53.2146 315.7281 0001516 87.6245 272.4921 15.08835844 00
| Epoch (UTC): | 25 May 2026 04:23:59 |
| Eccentricity: | 0.0001516 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 315.7281° |
| argument of perigee: | 87.6245° |
| revolutions per day: | 15.08835844 |
| mean anomaly at epoch: | 272.4921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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