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 68373U 26145.50832961 +.00000000 +00000-0 +31694-3 0 00008
2 68373 82.2970 37.6214 0004797 177.6283 182.5011 15.85378661 09
| Epoch (UTC): | 25 May 2026 12:11:59 |
| Eccentricity: | 0.0004797 |
| inclination: | 82.2970° |
| perigee height: | 312 km |
| apogee height: | 318 km |
| right ascension of ascending node: | 37.6214° |
| argument of perigee: | 177.6283° |
| revolutions per day: | 15.85378661 |
| mean anomaly at epoch: | 182.5011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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