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 67000U 26145.16582171 +.00000000 +00000-0 +43588-3 0 00006
2 67000 97.6377 221.4402 0016176 85.4294 274.8780 15.07297702 08
| Epoch (UTC): | 25 May 2026 03:58:46 |
| Eccentricity: | 0.0016176 |
| inclination: | 97.6377° |
| perigee height: | 533 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 221.4402° |
| argument of perigee: | 85.4294° |
| revolutions per day: | 15.07297702 |
| mean anomaly at epoch: | 274.8780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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