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 67602U 26145.45063622 +.00000000 +00000-0 +50453-3 0 00000
2 67602 97.2846 210.6619 0000568 193.1366 166.9862 15.33457333 07
| Epoch (UTC): | 25 May 2026 10:48:54 |
| Eccentricity: | 0.0000568 |
| inclination: | 97.2846° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.6619° |
| argument of perigee: | 193.1366° |
| revolutions per day: | 15.33457333 |
| mean anomaly at epoch: | 166.9862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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