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 51879U 26145.35445992 +.00000000 +00000-0 +54210-3 0 00007
2 51879 53.2126 14.9576 0001317 99.3954 260.7187 15.08799034 01
| Epoch (UTC): | 25 May 2026 08:30:25 |
| Eccentricity: | 0.0001317 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 14.9576° |
| argument of perigee: | 99.3954° |
| revolutions per day: | 15.08799034 |
| mean anomaly at epoch: | 260.7187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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