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 67896U 26145.37677977 +.00000000 +00000-0 +85583-5 0 00004
2 67896 97.2850 78.9478 0001471 96.5437 263.5974 15.33424446 01
| Epoch (UTC): | 25 May 2026 09:02:33 |
| Eccentricity: | 0.0001471 |
| inclination: | 97.2850° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.9478° |
| argument of perigee: | 96.5437° |
| revolutions per day: | 15.33424446 |
| mean anomaly at epoch: | 263.5974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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