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 67820U 26145.50459469 +.00000000 +00000-0 +60227-3 0 00006
2 67820 97.2861 333.6083 0001758 94.2949 265.8495 15.33447545 02
| Epoch (UTC): | 25 May 2026 12:06:36 |
| Eccentricity: | 0.0001758 |
| inclination: | 97.2861° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.6083° |
| argument of perigee: | 94.2949° |
| revolutions per day: | 15.33447545 |
| mean anomaly at epoch: | 265.8495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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