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 51781U 26145.28636988 +.00000000 +00000-0 +65372-4 0 00000
2 51781 53.2128 355.2259 0001314 90.7136 269.4007 15.08831279 03
| Epoch (UTC): | 25 May 2026 06:52:22 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 355.2259° |
| argument of perigee: | 90.7136° |
| revolutions per day: | 15.08831279 |
| mean anomaly at epoch: | 269.4007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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