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 62432U 26144.94430877 +.00000000 +00000-0 +97625-3 0 00001
2 62432 53.1604 338.2494 0001065 88.2600 271.8523 15.30205609 06
| Epoch (UTC): | 24 May 2026 22:39:48 |
| Eccentricity: | 0.0001065 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.2494° |
| argument of perigee: | 88.2600° |
| revolutions per day: | 15.30205609 |
| mean anomaly at epoch: | 271.8523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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