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 67728U 26145.61605840 +.00000000 +00000-0 +41491-3 0 00003
2 67728 97.2861 199.1105 0000478 92.9549 267.1749 15.33452276 02
| Epoch (UTC): | 25 May 2026 14:47:07 |
| Eccentricity: | 0.0000478 |
| inclination: | 97.2861° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 199.1105° |
| argument of perigee: | 92.9549° |
| revolutions per day: | 15.33452276 |
| mean anomaly at epoch: | 267.1749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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