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 67893U 26145.37133884 +.00000000 +00000-0 +55703-3 0 00004
2 67893 97.2831 78.9544 0001868 82.1330 278.0125 15.33482754 09
| Epoch (UTC): | 25 May 2026 08:54:43 |
| Eccentricity: | 0.0001868 |
| inclination: | 97.2831° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.9544° |
| argument of perigee: | 82.1330° |
| revolutions per day: | 15.33482754 |
| mean anomaly at epoch: | 278.0125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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