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 67688U 26144.99828978 +.00000000 +00000-0 +68185-3 0 00006
2 67688 51.6294 49.9725 0009763 98.1989 262.0112 15.60112167 03
| Epoch (UTC): | 24 May 2026 23:57:32 |
| Eccentricity: | 0.0009763 |
| inclination: | 51.6294° |
| perigee height: | 381 km |
| apogee height: | 394 km |
| right ascension of ascending node: | 49.9725° |
| argument of perigee: | 98.1989° |
| revolutions per day: | 15.60112167 |
| mean anomaly at epoch: | 262.0112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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