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 68409U 26145.59773080 +.00000000 +00000-0 +32472-3 0 00008
2 68409 97.4042 26.5935 0015873 79.8034 280.4990 15.18896327 02
| Epoch (UTC): | 25 May 2026 14:20:43 |
| Eccentricity: | 0.0015873 |
| inclination: | 97.4042° |
| perigee height: | 498 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 26.5935° |
| argument of perigee: | 79.8034° |
| revolutions per day: | 15.18896327 |
| mean anomaly at epoch: | 280.4990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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