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 67652U 26145.34829631 +.00000000 +00000-0 +55554-3 0 00000
2 67652 97.2853 178.6447 0000992 249.6353 110.4783 15.33444893 09
| Epoch (UTC): | 25 May 2026 08:21:32 |
| Eccentricity: | 0.0000992 |
| inclination: | 97.2853° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.6447° |
| argument of perigee: | 249.6353° |
| revolutions per day: | 15.33444893 |
| mean anomaly at epoch: | 110.4783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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