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 67253U 26144.20436862 +.00000000 +00000-0 +12475-3 0 00006
2 67253 97.0839 221.8356 0006286 279.0840 80.9707 15.60752812 08
| Epoch (UTC): | 24 May 2026 04:54:17 |
| Eccentricity: | 0.0006286 |
| inclination: | 97.0839° |
| perigee height: | 381 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 221.8356° |
| argument of perigee: | 279.0840° |
| revolutions per day: | 15.60752812 |
| mean anomaly at epoch: | 80.9707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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