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 53877U 26145.62984735 +.00000000 +00000-0 +12991-3 0 00000
2 53877 98.5533 144.0643 0005940 108.5869 251.5960 14.32701049 01
| Epoch (UTC): | 25 May 2026 15:06:58 |
| Eccentricity: | 0.0005940 |
| inclination: | 98.5533° |
| perigee height: | 778 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 144.0643° |
| argument of perigee: | 108.5869° |
| revolutions per day: | 14.32701049 |
| mean anomaly at epoch: | 251.5960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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