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 62864U 26145.28256356 +.00000000 +00000-0 +41761-3 0 00006
2 62864 53.1588 134.0760 0001444 81.1587 278.9577 15.30222033 08
| Epoch (UTC): | 25 May 2026 06:46:53 |
| Eccentricity: | 0.0001444 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 134.0760° |
| argument of perigee: | 81.1587° |
| revolutions per day: | 15.30222033 |
| mean anomaly at epoch: | 278.9577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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