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 65872U 26145.40616258 +.00000000 +00000-0 +74577-3 0 00004
2 65872 53.1599 297.6685 0001531 77.5477 282.5695 15.30210766 00
| Epoch (UTC): | 25 May 2026 09:44:52 |
| Eccentricity: | 0.0001531 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 297.6685° |
| argument of perigee: | 77.5477° |
| revolutions per day: | 15.30210766 |
| mean anomaly at epoch: | 282.5695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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