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 67897U 26145.38223109 +.00000000 +00000-0 +47288-3 0 00008
2 67897 97.2850 78.9408 0001743 101.0929 259.0510 15.33444965 09
| Epoch (UTC): | 25 May 2026 09:10:24 |
| Eccentricity: | 0.0001743 |
| inclination: | 97.2850° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.9408° |
| argument of perigee: | 101.0929° |
| revolutions per day: | 15.33444965 |
| mean anomaly at epoch: | 259.0510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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