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 67964U 26145.60844522 +.00000000 +00000-0 +45750-3 0 00008
2 67964 97.2833 155.5760 0001796 96.6862 263.4586 15.33445049 07
| Epoch (UTC): | 25 May 2026 14:36:09 |
| Eccentricity: | 0.0001796 |
| inclination: | 97.2833° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 155.5760° |
| argument of perigee: | 96.6862° |
| revolutions per day: | 15.33445049 |
| mean anomaly at epoch: | 263.4586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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