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 67536U 26145.63334087 +.00000000 +00000-0 +41750-3 0 00002
2 67536 97.2879 32.6457 0001939 90.6723 269.4742 15.33453874 04
| Epoch (UTC): | 25 May 2026 15:12:00 |
| Eccentricity: | 0.0001939 |
| inclination: | 97.2879° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.6457° |
| argument of perigee: | 90.6723° |
| revolutions per day: | 15.33453874 |
| mean anomaly at epoch: | 269.4742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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