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 67661U 26145.54678029 +.00000000 +00000-0 +50990-3 0 00004
2 67661 97.2854 178.8335 0000579 137.3822 222.7466 15.33459068 08
| Epoch (UTC): | 25 May 2026 13:07:21 |
| Eccentricity: | 0.0000579 |
| inclination: | 97.2854° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.8335° |
| argument of perigee: | 137.3822° |
| revolutions per day: | 15.33459068 |
| mean anomaly at epoch: | 222.7466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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