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 67696U 26145.55571573 +.00000000 +00000-0 +49333-3 0 00008
2 67696 97.2843 257.1802 0000636 93.2688 266.8628 15.33450491 08
| Epoch (UTC): | 25 May 2026 13:20:13 |
| Eccentricity: | 0.0000636 |
| inclination: | 97.2843° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1802° |
| argument of perigee: | 93.2688° |
| revolutions per day: | 15.33450491 |
| mean anomaly at epoch: | 266.8628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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