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 53700U 26145.35946477 +.00000000 +00000-0 +37688-4 0 00007
2 53700 53.2154 259.5625 0001192 85.2748 274.8381 15.08836737 09
| Epoch (UTC): | 25 May 2026 08:37:37 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 259.5625° |
| argument of perigee: | 85.2748° |
| revolutions per day: | 15.08836737 |
| mean anomaly at epoch: | 274.8381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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