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 67714U 26145.58019602 +.00000000 +00000-0 +61464-3 0 00001
2 67714 97.2849 257.1462 0001374 77.9628 282.1769 15.33409978 01
| Epoch (UTC): | 25 May 2026 13:55:28 |
| Eccentricity: | 0.0001374 |
| inclination: | 97.2849° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 257.1462° |
| argument of perigee: | 77.9628° |
| revolutions per day: | 15.33409978 |
| mean anomaly at epoch: | 282.1769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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