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 67697U 26145.56387056 +.00000000 +00000-0 +51464-3 0 00009
2 67697 97.2846 257.1674 0000226 213.4982 146.6246 15.33448594 09
| Epoch (UTC): | 25 May 2026 13:31:58 |
| Eccentricity: | 0.0000226 |
| inclination: | 97.2846° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1674° |
| argument of perigee: | 213.4982° |
| revolutions per day: | 15.33448594 |
| mean anomaly at epoch: | 146.6246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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