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 63377U 26145.18428703 +.00000000 +00000-0 +51797-3 0 00002
2 63377 53.1584 56.9705 0001085 87.1331 272.9794 15.30209394 09
| Epoch (UTC): | 25 May 2026 04:25:22 |
| Eccentricity: | 0.0001085 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 56.9705° |
| argument of perigee: | 87.1331° |
| revolutions per day: | 15.30209394 |
| mean anomaly at epoch: | 272.9794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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