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 51877U 26145.03060681 +.00000000 +00000-0 +29359-4 0 00005
2 51877 53.2139 16.4113 0001295 81.9525 278.1614 15.08842525 05
| Epoch (UTC): | 25 May 2026 00:44:04 |
| Eccentricity: | 0.0001295 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 16.4113° |
| argument of perigee: | 81.9525° |
| revolutions per day: | 15.08842525 |
| mean anomaly at epoch: | 278.1614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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