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 67532U 26145.40766856 +.00000000 +00000-0 +75252-3 0 00000
2 67532 97.2865 32.4983 0002394 98.5859 261.5655 15.33449961 08
| Epoch (UTC): | 25 May 2026 09:47:02 |
| Eccentricity: | 0.0002394 |
| inclination: | 97.2865° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.4983° |
| argument of perigee: | 98.5859° |
| revolutions per day: | 15.33449961 |
| mean anomaly at epoch: | 261.5655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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