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 67323U 26145.28913906 +.00000000 +00000-0 +74775-3 0 00003
2 67323 42.9995 252.6847 0000901 284.8596 75.2156 15.27594436 09
| Epoch (UTC): | 25 May 2026 06:56:21 |
| Eccentricity: | 0.0000901 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 252.6847° |
| argument of perigee: | 284.8596° |
| revolutions per day: | 15.27594436 |
| mean anomaly at epoch: | 75.2156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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