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 65482U 26144.74999845 +.00000000 +00000-0 +75446-3 0 00009
2 65482 53.1580 264.5237 0001134 127.6271 232.4834 15.34410546 02
| Epoch (UTC): | 24 May 2026 17:59:59 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1580° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 264.5237° |
| argument of perigee: | 127.6271° |
| revolutions per day: | 15.34410546 |
| mean anomaly at epoch: | 232.4834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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