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 67698U 26145.55843319 +.00000000 +00000-0 +55681-3 0 00003
2 67698 97.2848 257.1796 0000543 95.0517 265.0788 15.33452046 01
| Epoch (UTC): | 25 May 2026 13:24:08 |
| Eccentricity: | 0.0000543 |
| inclination: | 97.2848° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1796° |
| argument of perigee: | 95.0517° |
| revolutions per day: | 15.33452046 |
| mean anomaly at epoch: | 265.0788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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