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 62868U 26145.26565332 +.00000000 +00000-0 -72097-4 0 00003
2 62868 53.1573 133.9650 0001217 61.1720 298.9403 15.30199820 04
| Epoch (UTC): | 25 May 2026 06:22:32 |
| Eccentricity: | 0.0001217 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.9650° |
| argument of perigee: | 61.1720° |
| revolutions per day: | 15.30199820 |
| mean anomaly at epoch: | 298.9403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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