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 62824U 26145.47689125 +.00000000 +00000-0 +65811-3 0 00009
2 62824 53.1585 313.0110 0001095 76.7214 283.3908 15.30212743 03
| Epoch (UTC): | 25 May 2026 11:26:43 |
| Eccentricity: | 0.0001095 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.0110° |
| argument of perigee: | 76.7214° |
| revolutions per day: | 15.30212743 |
| mean anomaly at epoch: | 283.3908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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