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 51776U 26145.56236920 +.00000000 +00000-0 +10973-3 0 00003
2 51776 53.2132 354.0235 0001293 91.4404 268.6737 15.08838737 02
| Epoch (UTC): | 25 May 2026 13:29:48 |
| Eccentricity: | 0.0001293 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 354.0235° |
| argument of perigee: | 91.4404° |
| revolutions per day: | 15.08838737 |
| mean anomaly at epoch: | 268.6737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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