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 68533U 26145.25914828 +.00000000 +00000-0 +75918-3 0 00008
2 68533 53.1582 132.5006 0001195 90.9557 269.1583 15.34396476 01
| Epoch (UTC): | 25 May 2026 06:13:10 |
| Eccentricity: | 0.0001195 |
| inclination: | 53.1582° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 132.5006° |
| argument of perigee: | 90.9557° |
| revolutions per day: | 15.34396476 |
| mean anomaly at epoch: | 269.1583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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