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 67576U 26145.14086641 +.00000000 +00000-0 +79723-3 0 00003
2 67576 97.2853 205.5202 0001100 90.8873 269.2496 15.33445276 08
| Epoch (UTC): | 25 May 2026 03:22:50 |
| Eccentricity: | 0.0001100 |
| inclination: | 97.2853° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.5202° |
| argument of perigee: | 90.8873° |
| revolutions per day: | 15.33445276 |
| mean anomaly at epoch: | 269.2496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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