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 68387U 26145.42002812 +.00000000 +00000-0 +57949-3 0 00009
2 68387 97.2837 287.9656 0001155 108.1749 251.9620 15.33459008 08
| Epoch (UTC): | 25 May 2026 10:04:50 |
| Eccentricity: | 0.0001155 |
| inclination: | 97.2837° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 287.9656° |
| argument of perigee: | 108.1749° |
| revolutions per day: | 15.33459008 |
| mean anomaly at epoch: | 251.9620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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