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 68483U 26145.62076639 +.00000000 +00000-0 +45260-3 0 00009
2 68483 97.7623 104.3101 0003801 32.5921 327.5532 14.92545689 09
| Epoch (UTC): | 25 May 2026 14:53:54 |
| Eccentricity: | 0.0003801 |
| inclination: | 97.7623° |
| perigee height: | 587 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 104.3101° |
| argument of perigee: | 32.5921° |
| revolutions per day: | 14.92545689 |
| mean anomaly at epoch: | 327.5532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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