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 52877U 26145.10099650 +.00000000 +00000-0 +17092-3 0 00002
2 52877 53.2139 31.1039 0001750 88.2562 271.8630 15.08831567 06
| Epoch (UTC): | 25 May 2026 02:25:26 |
| Eccentricity: | 0.0001750 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 31.1039° |
| argument of perigee: | 88.2562° |
| revolutions per day: | 15.08831567 |
| mean anomaly at epoch: | 271.8630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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