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 67143U 26145.12849262 +.00000000 +00000-0 +40087-3 0 00008
2 67143 51.9005 95.1322 0000835 66.6705 293.4345 14.79958926 01
| Epoch (UTC): | 25 May 2026 03:05:01 |
| Eccentricity: | 0.0000835 |
| inclination: | 51.9005° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 95.1322° |
| argument of perigee: | 66.6705° |
| revolutions per day: | 14.79958926 |
| mean anomaly at epoch: | 293.4345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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