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 67554U 26145.43863792 +.00000000 +00000-0 +14312-2 0 00003
2 67554 97.2861 34.1332 0001844 84.6454 275.5021 15.75250161 01
| Epoch (UTC): | 25 May 2026 10:31:38 |
| Eccentricity: | 0.0001844 |
| inclination: | 97.2861° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 34.1332° |
| argument of perigee: | 84.6454° |
| revolutions per day: | 15.75250161 |
| mean anomaly at epoch: | 275.5021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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