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 67402U 26145.25890275 +.00000000 +00000-0 +13902-3 0 00006
2 67402 97.4565 144.4608 0005047 64.1904 295.9850 15.17555265 04
| Epoch (UTC): | 25 May 2026 06:12:49 |
| Eccentricity: | 0.0005047 |
| inclination: | 97.4565° |
| perigee height: | 510 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 144.4608° |
| argument of perigee: | 64.1904° |
| revolutions per day: | 15.17555265 |
| mean anomaly at epoch: | 295.9850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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