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 67707U 26145.27838029 +.00000000 +00000-0 +72616-3 0 00002
2 67707 97.2847 256.9448 0000907 100.6516 259.4829 15.33466547 02
| Epoch (UTC): | 25 May 2026 06:40:52 |
| Eccentricity: | 0.0000907 |
| inclination: | 97.2847° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 256.9448° |
| argument of perigee: | 100.6516° |
| revolutions per day: | 15.33466547 |
| mean anomaly at epoch: | 259.4829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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