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 62858U 26145.35164985 +.00000000 +00000-0 +79283-3 0 00003
2 62858 53.1602 132.3794 0001542 71.8698 288.2472 15.34370293 08
| Epoch (UTC): | 25 May 2026 08:26:22 |
| Eccentricity: | 0.0001542 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 132.3794° |
| argument of perigee: | 71.8698° |
| revolutions per day: | 15.34370293 |
| mean anomaly at epoch: | 288.2472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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