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 63367U 26145.20530148 +.00000000 +00000-0 +51913-3 0 00001
2 63367 53.1577 67.0266 0001090 84.5051 275.6074 15.30210554 02
| Epoch (UTC): | 25 May 2026 04:55:38 |
| Eccentricity: | 0.0001090 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 67.0266° |
| argument of perigee: | 84.5051° |
| revolutions per day: | 15.30210554 |
| mean anomaly at epoch: | 275.6074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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