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 68286U 26144.81872822 +.00000000 +00000-0 +72959-3 0 00003
2 68286 53.1614 324.4256 0000733 106.0062 254.1021 15.34404576 00
| Epoch (UTC): | 24 May 2026 19:38:58 |
| Eccentricity: | 0.0000733 |
| inclination: | 53.1614° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 324.4256° |
| argument of perigee: | 106.0062° |
| revolutions per day: | 15.34404576 |
| mean anomaly at epoch: | 254.1021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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