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 67883U 26145.53177237 +.00000000 +00000-0 +51040-3 0 00001
2 67883 97.2853 79.0424 0001699 98.5093 261.6342 15.33455203 08
| Epoch (UTC): | 25 May 2026 12:45:45 |
| Eccentricity: | 0.0001699 |
| inclination: | 97.2853° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 79.0424° |
| argument of perigee: | 98.5093° |
| revolutions per day: | 15.33455203 |
| mean anomaly at epoch: | 261.6342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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