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 65483U 26144.83936536 +.00000000 +00000-0 +98409-3 0 00002
2 65483 53.1562 264.3713 0000604 107.5384 252.5683 15.30213501 06
| Epoch (UTC): | 24 May 2026 20:08:41 |
| Eccentricity: | 0.0000604 |
| inclination: | 53.1562° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 264.3713° |
| argument of perigee: | 107.5384° |
| revolutions per day: | 15.30213501 |
| mean anomaly at epoch: | 252.5683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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