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 67353U 26145.35144488 +.00000000 +00000-0 +76998-3 0 00004
2 67353 43.0042 154.5297 0001719 246.7761 113.2909 15.27594193 04
| Epoch (UTC): | 25 May 2026 08:26:04 |
| Eccentricity: | 0.0001719 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.5297° |
| argument of perigee: | 246.7761° |
| revolutions per day: | 15.27594193 |
| mean anomaly at epoch: | 113.2909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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