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 67278U 26145.14476226 +.00000000 +00000-0 +28023-3 0 00001
2 67278 97.3902 220.0802 0016407 88.9498 271.3618 15.22350318 08
| Epoch (UTC): | 25 May 2026 03:28:27 |
| Eccentricity: | 0.0016407 |
| inclination: | 97.3902° |
| perigee height: | 487 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 220.0802° |
| argument of perigee: | 88.9498° |
| revolutions per day: | 15.22350318 |
| mean anomaly at epoch: | 271.3618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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