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 68466U 26144.78056654 +.00000000 +00000-0 +29373-3 0 00008
2 68466 97.4469 103.4579 0007081 145.8461 214.3230 15.17234587 03
| Epoch (UTC): | 24 May 2026 18:44:00 |
| Eccentricity: | 0.0007081 |
| inclination: | 97.4469° |
| perigee height: | 509 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 103.4579° |
| argument of perigee: | 145.8461° |
| revolutions per day: | 15.17234587 |
| mean anomaly at epoch: | 214.3230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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