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 67663U 26145.34285997 +.00000000 +00000-0 +34947-3 0 00006
2 67663 97.2848 178.6529 0001184 96.0949 264.0428 15.33450770 08
| Epoch (UTC): | 25 May 2026 08:13:43 |
| Eccentricity: | 0.0001184 |
| inclination: | 97.2848° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.6529° |
| argument of perigee: | 96.0949° |
| revolutions per day: | 15.33450770 |
| mean anomaly at epoch: | 264.0428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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