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 67657U 26145.05736800 +.00000000 +00000-0 +14287-3 0 00006
2 67657 97.2863 178.2752 0000159 284.9080 75.2145 15.33438319 00
| Epoch (UTC): | 25 May 2026 01:22:36 |
| Eccentricity: | 0.0000159 |
| inclination: | 97.2863° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.2752° |
| argument of perigee: | 284.9080° |
| revolutions per day: | 15.33438319 |
| mean anomaly at epoch: | 75.2145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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