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 62442U 26145.53278220 +.00000000 +00000-0 +51911-3 0 00008
2 62442 53.1609 338.3576 0001372 94.9574 265.1584 15.30211799 09
| Epoch (UTC): | 25 May 2026 12:47:12 |
| Eccentricity: | 0.0001372 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.3576° |
| argument of perigee: | 94.9574° |
| revolutions per day: | 15.30211799 |
| mean anomaly at epoch: | 265.1584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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