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 67131U 26145.14197948 +.00000000 +00000-0 +17934-3 0 00009
2 67131 97.4735 223.2153 0007145 38.1639 322.0101 15.21421174 07
| Epoch (UTC): | 25 May 2026 03:24:27 |
| Eccentricity: | 0.0007145 |
| inclination: | 97.4735° |
| perigee height: | 497 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 223.2153° |
| argument of perigee: | 38.1639° |
| revolutions per day: | 15.21421174 |
| mean anomaly at epoch: | 322.0101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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