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 67725U 26145.42843038 +.00000000 +00000-0 +70821-3 0 00001
2 67725 97.2871 198.9063 0000164 221.4330 138.6900 15.33489388 04
| Epoch (UTC): | 25 May 2026 10:16:56 |
| Eccentricity: | 0.0000164 |
| inclination: | 97.2871° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.9063° |
| argument of perigee: | 221.4330° |
| revolutions per day: | 15.33489388 |
| mean anomaly at epoch: | 138.6900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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